LU E->< LU LU > LUG LU 2: OLU
>-:i:
o-LU E. G LU LUz
L'-.o
z
o
Del
NAVAL SHIP RESEARCH AND DEVELOPMENT CENTER
Washington, D C. 20034
Onderafdel
sbouwkjndeT .. nische Hoqeschool,
D)CUMEN!ATIE
J: 4'f
if/
DATUM:
I/4S j;øI-,-).
AN APPLICATION OF LINEARIZED THEORY TO WATER /F*i.--.
ENTRY AND WATER EXIT PROBLEM PART 2 (WITH VENTILATION)
by B. Yim
This docunient has been approved for public release and sale; its distri-bution is unlimited.
DEPARTMENT OF HYDROMECHANICS RESEARCH AND DEVELOPMENT REPORT
July 1970 Report 3171
The Naval Ship Research and Development Center is a U.S. Navycenter for laboratory effort directed at achieving improved sea and air vehicles. lt was formed in March 1967 by merging the David Taylor Model F3asin at Carderock, Maryland and the Marine Engineering Laboratory (now
Naval Ship R &. D Laboratory) at Annapolis, Maryland. The Mine Defense Laboratory (now Naval
Ship R &. D Laboratory) Panama City, Florida became part of the Center in November 1967.
Naval Ship Research and Development Center
Washington, D.C. 20007 * REPORTORIGINATOR SHIP CONCEPT RESEARCH OFFICE 0H00 DEPARTMENT OF ELECTRICAL EN GIN EE RIN G ARDO DEPARTMENT OF MACH IRY TECHNOLOGY ASSO DEPARTMENT OF MATERIALS TECHNOLOGY HAYO DEPARTEtNT OF APPLIED SCIENCE AYOS SYSTEMS DEVELOPMENT OFFICE 0H01 NSRDL ANNAPOLIS CO4HANGING OFFICER TECHNICAL DIRECTOR
H
H
H
H
MAJOR NSRDC ORGANIZATIONAL COMPONENTS
DE lIE LORMENT PROJECT OFFICES OlIDO SO. 80.90
*
DEPARTMENT OF 11V DR0HECH AN IC S 500 N SR DC CARD ER OC K C084.IAN DER TECHNICAL DIRECTOR DEPARTMENT DF STRUCTURAL MECHANICS 700 DEPARTMENT OF APPLIED MATHEMATICS 800 DEPARTMENT OF ACOUSTICS AND VIBRATION900 L,PARTMENT OF AERODYNAMICS 600 N ORO L PANAMA CITY C08*AANDING OFFICER TECHNICAL DIRECTOR
H
H
H
DEPARTMENT 0F OCEAN TECHNOLOGY P710 DEPARTMENT 0F MINE COUNTERMEASURES P720 DEPARTMENT OF AIRBORNE MINE COUNTERMEASURES P730 ¡ DEPARTMENT 0F INSHOREI WARFARE AND TORPEDO
DEFENSE P710
DEPARTMENT OF THE NAVY
NAVAL SHIP RESEARCH AND DEVELOPMENT
CENTER
Washington, D.C. 20034
AN APPLICATION OF LINEARIZED THEORY TO WATER
ENTRY AND WATER EXIT PROBLEM PART 2 (WITH VENTILATION)
by
B. Yim
This document has been approved for public release and sale; its distri-bution is unlimited.
TABLE OF CONTENTS Page ABSTRACT 1 ADMINISTRATIVE INFORMATION i INTRODUCTION 1 FORMULATION OF PROBLEM 3 CONFORMAL MAPPING S
GENERAL TECHNIQUE FOR OBTAINING SOLUTIONS 6
WATER ENTRY OF A NONSYMMETRICAL WEDGE 8
WATER ENTRY OF A FLAT PLATE WITH LEADING EDGE CAVITY 10
BASE-VENTED SYMMETRICAL WEDGE 13
DISCUSSION 17 ACKNOWLEDGMENTS 19 REFERENCES 28 LIST OF FIGURES Figure Figure Figure 1 2 3 - Nonsymmetrical Wedge - Ventilating Flat Plate
- Base-Vented Symntetrical Wedge
P ag e
20 21 22
Figure 4 - Pressure Distribution on the Pressure Side of a
Nonsymmetrical Wedge Entering Water 23
Figure 5 - Pressure Distribution on the Suction Side of a
Nonsymmetrical Wedge Entering Water 24
Figure 6 - Effect of Changing Angle on Pressure Distribution on
the Pressure Side of a Nonsymmetrical Wedge 25
Figure 7 - Pressure Distribution on a Vented Flat Plate Entering a
Water Surface 25
Figure 8 - Drag and Lift Coefficients of Nonsyrnrnetrical Wedges and
Ventilated Flat Plates Entering Water 26
Figure 9 - Pressure Distribution on a Base-Vented Thin Wedge
Entering the Water at F =
r 26
Figure 10 - Drag Coefficient of a Base-Vented Symmetrical Wedge
Page
Figure 11 - Cavity Shape of a Ventilated Flat Plate Entering
Water
27
Table i - Singularities of w and w
NOTATION A0, A., A I Coefficients to be determined
A,B
f C Chord length D DragK Given in Equations (10) and (13a)
p Pressure
t Time
u x-component of velocity of water particle
V Foil speed
y y-component of velocity of water particle
w Complex velocity
x, y Rectangular coordinate system
z
=x+iy
0 a2 Wedge angle
a Angle of attack of flat plate
Transformed coordinate
p Density of water
Potential
Subscripts t, x, y, and designate partial differentations with respect to t, x, y, and , respectively.
*
References are listed on page 28. ABSTRACT
A conformal mapping technique is used to analyze
two-dimensional thin foils entering a water surface vertically
with ventilations. Boundary conditions are linearized, and the gravity effect is neglected. Flow fields, pressure
dis-tributions, and drags are given in closed forms for an in-finite nonsymmetrical wedge, an inin-finite flat plate with
ventilation from the leading edge, and a finite base-vented
symmetrical wedge.
ADMINISTRATIVE INFORMATION
The work reported herein was carried out under the Naval Ship Research and Development Center (NSRDC) General Hydromechanics Research Program
Pro-ject SR 0090101 and the NSRDC in-house Independent Exploratory Development
Program Project ZFXX412001.
INTRODUCTION
Reference 1* treated the two-dimensional linearized hydrodynamic problem of a wedge penetrating a heavy water surface with a constant
velocity. The infinite Froude number approximation was found to be good for Froude numbers (VI j/E) of 3 or larger. The infinite Froude number approximation simplifies the boundary conditions considerably, i.e., a zero
acceleration potential on the free surface. This simplified model is used here for the more complicated problems dealt with in this report.
The water entry of a wedge or a foil with a finite chord may be
con-sidered in two stages: (1) the first stage between the time the leading
edges touch the water surface and the time the trailing edge enters the water and (2) the second stage after the trailing edge enters the water and
a trailing edge cavity is formed and entrained behind. Since the nature
of the problem is different for these two states, the solution to the
problem may be dealt with in two steps.
The present study used the method of conformal mapping to
and a base-ventilated symmetrical wedge. Only the first stage was treated
for the first two configurations because of the complexity involved. Only
the second stage was investigated for the symmetrical wedge since the
so-lution for the first stage had already been reported.1
Generally, the approach is to solve first the time derivatives of
the complex velocity w in the transformed half-plane for given boundary
conditions along the real axis. The conformal mapping is a function of the
coordinate of the physical plane and the time t. Unknown coefficients associated with w are determined by matching the boundary conditions of
the complex velocity w and the pressure. The pressure is obtained by
inte-grating w with respect to the physical coordinates.
The solutions of flow field, pressure, and drag are given in closed
forms for all the configurations treated here. This was possible because
of the following three facts:
The configurations all have straight sides which make the boundary
conditions for w all zeros in the transformed plane, unlike the cases of
cambered foils.
For the problems of the first-stage entry, the complex velocity w is
a function of time only through the time-dependent transformed coordinates;
for the problem of the second-stage entry, the symmetry of the problem
helps the simplification.
The numbers of juncture points are small enough for closed-form
inte-grals.
It was felt that this investigation would be extremely helpful in under-standing the physical behavior of flows due to impinging blades of partially
submerged propellers or to similar water entry with ventilation. Numerous linear theoretical treatments of water entry have been published,1 but a
literature search failed to find a linear treatment of water entry problems with ventilation. The investigation reported here was motivated by the potential application to partially submerged propellers for high-speed, high-power craft; such results will also contribute to an understanding of
Initially
FORMULATION OF PROBLEM
The free surface at time t < 0 is undisturbed and represented by
y = 0. The y-axis is vertically upward and the x-axis is on the undisturbed
free surface such that the conventional rectangular coordinate system 0-xy
is formed. Consider a two-dimensional foil with chord c
x = f(y + Vt) , O < y + Vt < c (1)
penetrating through the water surface vertically with speed V, touching the origin O at t = 0. Then there exists in the water the potential
x,y,t) which satisfies
+c
=0
(2)xx yy
at any time. On the free surface, if an infinite Froude number approxi-mation is used,
=
°'i
'
= 0within the linear approximation. From the Bernoulli equation, the
pertur-bation pressure p can be represented by
p=-ppt
(3)Thus
= O (4)
on the cavity.
Within the linear approximation, this condition can be applied on the y-axis instead of the unknown cavity surface when the foil is thin.2
On the foil, the relative normal velocity is zero. Thus
X = V f (y + Vt)
on (5)
Q < y + Vt < c , x = O
= = O
At infinity,
decaying properly. Especially, for the water entry of a wedge1
Thus this is a mixed boundary value problem.
To solve this problem, Equation (2) is modified by differentiation
with respect to t From Equation (3) From Equation (4) From Equation (S) Let (7) = 2 1
2'
at 2 + y2\X +y/
+q
=0
txx tyy tx = 0 on y = 0ty = O on the cavity part of x = O
=v2
tx yy
on
O<y+Vt<1,x=0
w(x,y,t)=
-iq
tx ty
Then the problem for w is exactly the same as that for the complex potenti
with the real and imaginary boundary conditions available. This kind of
problem can be solved by the method used by Cheng and Rott3 within unknown
constants. To obtain a complete solution, a conformal mapping has first
to be set; then the analytic function w which satisfies its boundary con-dition should be found; and finally, the unknown constants must be
determined to satisfy the original boundary conditions for w and =
-(7a)
(3 a)
(S a)
CONFORMAL MAPPING
At time t, the physical boundary configuration where the boundary conditions are applied is approximated
by straight segments A BCD A as
in Figures 1 and 2. By the Schwartz-Christoffel transformation,4 thez = x + iy plane can be transformed to the ç = + in plane (Figure 3)
as
kç (8)
y/ç
-1
with the points B (z = + 0), D (z = 0), and C (z = -Vt i) mapped to ç = -1,
ç = 1, and ç = O respectively, where V indicates constant speed. The integration of Equation (1) leads to
1
z = K(ç2 1)2 + L (9)
Constants K and L will be determined by matching coordinates
r ç = 1, z = O ; hence L = O I (10) ç = O z = -Vti; hence K = -Vt Thus dz dç or
z = 2K/+ L
(12)transforms the z-plane to the ç-plane with the correspondence:
çV2
= (Vt)2z
(9a)
For problems of symmetrical wedges, only one-quarter of the physical plane may be needed as shown in Figure 4.
The mapping function
dz_
KThus it leads to
(14)
ç=O,
z=O
;henceL=O
ç = 1, z = -Vti; hence K = -iVt/2 (13a)
ç = a, z = (_\Tt + l)i;
a - ívt - i
2
(l3b)
Also from Equations (12) and (13)
fz
\2(:2a)
GENERAL TECHNIQUE FOR OBTAINING SOLUTIONS
The boundary conditions in the z-plane for w, which are analytic except at singular points on the boundary, do not change in the ç-plane on
the corresponding segments. The unique characteristic of the problems
concerned here is that the boundary conditions of w are all either real
parts or the imaginary parts of w. For the solution to this kind of problem in the ç-plane, a homogeneous solution must be found first; all
the given nonzero boundary values are replaced by zero, and the solution
is found for the same problem. For this, conditions at the juncture point must be specified. First it is reasonable to assume the Kutta condition4
at the trailing edge. At the leading edge there can be a certain
singu-larity as in the steady flow of a linear cavitating foil.5 At the joint
of the free surface and the cavity, there could be some singularity which
might indicate the possibility of spray phenomena. At infinity, the same behavior is assumed as that of the solutions for the wedge entry
w log
-2)
z - z
(1
z-z1
for a large
z.
Singularities of w and at the juncture points areIf the boundary values of w and juncture points in the c-plane are
not functions of t, w is a function of t only through r. Namely
wt w (15)
where = F (z, t) from the conformal transformation. Actually, from Equation (9)
2
- t
(16)
and from Equation (12)
2
-- t (17)
All problems treated in this report have homogeneous boundary
con-ditions for w
or w.
Thus the homogeneous solutions are our solutions.They have a form of3
q1 q2 q3 m
w=(+l)
(ç-1)
ç(A+A.ç «.ç)
ç o
it
mwhere q. is given one-half plus the integer or integers that can be used
to satisfy juncture conditions,
A are unknown coefficients that are functions of juncture points, and
m should be decided by the condition at .
TABLE i
Singularities of w and
(18)
w
Leading Edge of Wedge
Trailing Edge with Cavity Entrairunent
Juncture Point of Free Surface and Foil
At Infinity 1/ç l/ç2 log(ç-i) l/z2 l/(ç-l) l/z3 ----dç
The unknown coefficients are determined by matching boundary conditions of
w and the pressure; w is from
1.
ÇWt
w= j
w d= j
--dçThe pressure will be obtained from Equation (3) and
dz
= Re
J
w --- dWhen the boundary condition on the foil is an arbitrary function of y + Vt,
set a function
H
- U
-
i VHW u - i v
(21)
where H is the homogeneous solution; then the imaginary part of wt/H will be known everywhere on the real axis of the -p1ane.3 Thus, the solution for w can be written
w
W
t
H 1Hd
1Tl (22)-WATER ENTRY OF A NONSYMMETRICAL WEDGE
The problem of a symmetrical wedge has already been solved by using the Green function.1 The problem of the nonsymmetrical wedge will be a
little more general. Consider that a wedge whose two side planes respectively form angles a1 and a2 with the y-axis enters the water vertically with speed V. Then the boundary conditions on the wedge are
Thus
j-a2inü<y+Vt
x=-O
f (y + Vt) = ya1inü<yVt x=+0
f),t(>T +
Vt) = fyy = O in O < + Vt x 0 (24) (23)Hence a possible solution for w is obtainable from Equations (9) and (14) through (16) and the juncture conditions shown in Table 1
= 2 2 -
2(+l)
2(-l)
A +BR
-1) B- -+
AA-Bk
A+BI
(25)where A and B are unknown real coefficients to be determined by matching
conditions. From Equation (25) w =
J
w d i(B-A) /i . A+B Il+lo
+1
-
2 g l+ç) 2 log--)
(26)From the boundary conditions of Equations (23) and (25)
B- A
2A+ B
2--a2V/T
or = Re V VA- (a1 + a2), B= (a
-
a)-1
2i
The pressure will be obtained from Equations (3) and (20)
1 1 dz dz = - = Re
J
w -- d = ReJ
w d p t ç-.2
V
Trf(a1+
a2)ç+a2
-2_ç
ç-
I (a - a2)ç (a2 + a1) log
2
Tr 1
1
+Vlç2
(27)
when a2 a1 = a p 4 ç 4 l/f'Vt)2_ y2 = log = log
-
1+
yÇi?
-:;:-vt+
yaV2
2 log - Vt--
ono>y> -Vt
(29) y + Vtwhich was obtained previously.1
Thus the first term of the right-hand side of Equation (28) is due
to the nonsymnietry of the wedge. From Equation (26) this is clearly represented by a vorticity at ç=O with the strength proportional to
in the ç-plane.
This problem can also be easily solved for the complex velocity w = u - iv instead of w, since u is available everywhere on the boundary
of both the free surface and the wedge. The result is exactly the same as
that obtained here.
The drag coefficient of a nonsymmetrical wedge is from the
inte-WATER ENTRY OF A FLAT PLATE WITH LEADING EDGE CAVITY
Consider that a flat plate is entering the water surface vertically with a high speed V at an angle of attack a so that a cavity is formed
from the leading edge. When the flat plate has a finite chord c, the time
for the foil to fully enter the water is approximately c/(Vt). However, only the stage before full entrance will be considered here.
Since the pressure on the cavity is zero, the boundary values for w
gration of Equation (28)
D
_2
2-
(a1 + a2)
log 2 +(a2
2J
- a1)
p V Vt
The lift coefficient is
L 4
la
-ir I 2a
l
1 2 Vthomogeneous. From Equations (18), (19), (14), and (15) as well as the juncture conditions in Table 1, the solutions for w can be written as
i (A+A1
w =
ç
ç(ç-l) (ç+l) )t'ç(ç+l)
Coefficient A will be obtained from the boundary conditions of w which
can be obtained by integration of wç
C w
11
i w dç i i J ç 3ç i + + j/ç(ç-i-l)2A
A+A
+1 o 12'
2/
--
102'
ç - 1A +A
o 13+2"
+ (A_A)J/Ç+2A +
log o 1 °2)7k
2/
- (A0-A1) (31)The flow condition on the pressure side of the flat plate O < ç < i and the
quality of the pole at ç = i give
A + A 2)1v
o 1
For the condition on the cavity and the free surface, is obtained from Equations (3), (20), and (30)
i=-
=Ref
w
dz p ttdç
ç ' ki (A0+A1ç) Re tç(ç+1) ç(ç-l) dç (30)thus
A
= A ---aV
i o r
Therefore the pressure on the foil can be written
rp
-
Re2//i
a p
The drag is 0 1Vap
22
Vap
2 rrD p dy = Im 2yT
Ç d -Vt 6 1=im2iìJ
K/
d=2V'Vt JyÇÇdc
o = 2 }/Y Vt ¡+l) -
log ( + + i D - J. {8 - 23/
log (3 + 2 = 0.995 122
VapVt
TrRe['I2
A-A
-
A log o + i -1 1 o2'
2/
-3 1 + i A1-A0 3iog(
- l)Ñ
(33) t I°
\2V'
(Cont'd)To have p satisfy boundary conditions on the free surface jj>i and the
cavity 0>r>-1, it is necessary that
A -A =0
i o
(3
The approximate cavity shape of the ventilating flat plate can be obtained from y x = Re
J
w dy =J
u()
d =- Vtf u(a)
d -Vt O O O > > -1 using Equation (8).From Equations (31) and (35)
aV (2
VT'-
+ -1 2j"
J/(l-)
Re w = u = -
TIi - 3
TI
Thus the above integration leads to
z
2V(l-)
> ¡2(l+)
i (2)
tan 1 - 3 Vt TI-
y/(Vt)2
O > y > -VtBASE-VENTED SYMMETRICAL WEDGE
Up to this point, all the problems considered herein are related to the first stage before the full entrance of a wedge (or foil) of finite
chord.
After the full entrance, ventilation will be entrained from the trailing edge and sometimes from the leading edge. A water entry problem of this kind is extremely complicated for a general foil. However, when
the case is a symmetrical wedge entering the water surface vertically with
speed V, the problem becomes fairly simple.
1}
X
Vt
For the pressure
=
(c-l)
(-a)
where A and A1 are not functions of but possibly functions of t. Sub stituting =- z2/(Vt)2 from Equation (12a)
2 \) t
ti'A
+A
Z 2)Idt w =J
w dt =J
0(
(Vt) 2 2 (39) o°
(
(Vt)2 1) (Vt)2 ( (Vt)2 - a)Here the integral is imaginary when Vt
<Iy
at a given point on the y-axis. For -y + i > Vt > -y,Rew=cLV
(4 )This value is observed to be from the singularity at y =- Vt in the inte
grand of Equation (39). Thus
2V
Tr (A + A1) Vt dz=Re
Jwt-a_d
A +A
ç Vt ° (3=cV
(4In this case, the flow is symnietrical with respect to the wedge
axis. Therefore, only one-quarter of che physical plane or the z-plane
can be conveniently considered. The conformal mapping to the ç-plane is
already considered in Equations (il) through (13). The boundary conditions
of w are again homogeneous. Considering the behavior of singularities at
juncture points, including infinity, with Equations (7a), (11), (12), and (20), it is seen that w can be written
i(A
+ A1)
8)
p Vt p 2 A
2A
A +A
o i o -1 a tan log lo-A +-A
° log -vT
VtÏT
y+
V12
To have the pressure satisfy the boundary condition on the free surface
A =0
o
Therefore,
2 o.
V2 yii
Vtr
Thus the pressure on the wedge surface is given
=---lo
;ìii+
/ii+V2p
which satisfies all the boundary conditions.
When Vt = 1, a = O from Equation (13b). Then
p
- log
12
p
with =- z2,(vt This is already given in Equation (29).
For Vt - =), z x + (-Vt + y1)I, >1 2o.
1-y1+l
= - log
V2p
(42) (46) (47)which is the case of a steady cavitating wedge in an infinite medium
having a zero cavitation number.
The drag due to the wedge from the stage Vt/c = 1 will be - Vt + 1
D=2aJpdy
Thus where a =22
2cL V p = Im logi
J
--iog
=Vt
hm
EO
=um Vt
-
log logV+ VT
y-
yiT
(i-
-
-;-+ V(-a)(l-a
(c-l)
/i
D 2 2 p-
[log a +2-a2
]vt
log a ¿l-E
l-E--viJ(l-c)
p'i1
a aI
l-E
a
Vt
l\ )from Equation (13h). For a = O or Vt = 1.
D 4 = log 4
22
C (48)(49)
V+
dV-
yiT
logV-Vî
For Vt - either from Equation (48) or from the integration of Equation
(47),
V2a2
=(50)
which is the drag due to a two-dimensional cavitating wedge with the
cavi-tation number equal to zero2 in an infinite medium.
DISCUSSION
The pressure distributions on both sides of a nonsymmetrical wedge entering water for the wedge angles a1 + a = 0.2 and 0.1 radian are shown
in Figures 4a and Sa, and 4b and Sb, respectively, for various values of
- which are twice the angle between the y-axis and the centerline of the wedge. The effect of asymmetry comes from the first term on the
right-hand side of Equation (28), which is positive on the pressure side
of the wedge and negative on the suction side. The singularities of both the complex velocity and the pressure near the leading edge due to the asymmetry are like l/}/l-y/(Vt), while those for the symmetrical wedge are
logarithmic. Therefore, in the immediate vicinity of the leading edge,
this linearized theory has to be interpreted differently as in the case of
usual linearized-aerofoil theory.
Figure 6 shows the pressure distribution on the pressure side of a nonsymmetrical wedge for a certain angle a between the pressure side of the wedge and the y-axis, with varying angle ra (r < 1) between the suction
side of the wedge and the y-axis. It is interesting to see that when r decreases, the pressure increases very little on the pressure side.
Eventually, the suction side will cavitate at some small r like a flat
plate. Also note that there is very little difference between the pressure distributions on a cavitating flat plate and a symmetrical wedge, as shown
in Figure 7.
The leading edge singularities of the complex velocity and the
pressure for the ventilating flat plate entering water are like
(l-y/VtY4
The drag coefficient D/(1/2 p V2 Vt) and the lift coefficient L/(l/2 p V2 Vt) for a ventilating flat plate entering water are compared in Figure 8 with those of a nonsymmetrical wedge entering water for the
wedge angles a1 + a2 = 0.2 and 0.1 rädian. The drag coefficient of a
symmetrical wedge, i.e., when ci1 = a2 = a, is 1.75 a2 as shown in Equation
(49). But only one-half of this drag is due to a single side of the wedge.
When this is compared with the drag coefficient of the cavitating flat plate, the ratio of the latter to the former is 1.09, showing little
con-tribution from the difference in leading-edge singularities.
The change of the pressure distribution on base-vented symmetrical
wedges after full entry is shown in Figure 9. The increase of the pressure
22
rapidly approaches the steady state. The drag coefficient D/(l/2 p V a c)
of the base-vented symmetrical wedge is shown in Figure 10; the maximum drag increase of approximately 45 percent occurred for the period Vt
= C
from the time that the trailing edge was instantly on the mean freesur-face to the time when steady state was reached.
Under the present assumption that the cavity is from the free sur-face to the foil without any cavity closure or sursur-face sealing, there appeared to be no singularity for either w or p at the juncture point of
the free surface and the cavity. However, at the juncture point of the foil and the free surface, there was a logarithmic singularity for w.'
All the cases concerned here are particularly simple especially in
the c-plane. However, the results permit more physical information to be
easily extrapolated to aid in understanding actual complicated situations. Flow fields for a nonsymnietrical wedge and a cavitating flat plate can be obtained directly from Equations (26) and (31), respectively. For example,
the cavity shape due to the ventilating flat plate entering the water is
shown in Figure 11. Note that the cavity thickness is much smaller than the steady state case of a cavitating flat plate beneath the free surface.6 The behavior of the pressure field after the full entry of a finite
cavi-tating flat plate can be estimated from the case of the finite symmetrical
The solutions obtained thus far are for the problems of water
entry. A reversed application of the case of entry is possible for an
exiting foil that is not cavitating.7 However, the problem is much more complicated for an exiting, cavitating foil. This problem will be con-sidered in the near future.
ACKNOWLEDGMENTS
The author thanks Mr. J.B. Hadler, Dr. P.C. Pien, and Mr. H.M. Cheng for their interest and the valuable suggestions which contributed
A A -A (c)
txo
D = -a2V yi (b) E C-
IC = a1 B C OFigure 1 - Nonsymmetrical Wedg
A
A cO
A
(b) y e D4x=-av
(c) oA
4tx
B C DFigure 2 - Ventilating Flat Plate
B A
0
Y A co
-o
Dco c)Î
B E C DoeFigure 3 - Base-Vented Symmetrical P B X
Ax
t_o
(-Vt+I)
av
- Vt i X O E C0.8 O
-0.2
-0.4 -0.6-08
-1.0 y/vtFigure 4a - Wedge Angle
+
= 0.2 Radian
0.2 0.15 0.1 0.05
a2 --a
0.1 rad
Figure 4 - Pressure Distribution on the
Pressure
Side of a Nonsymmetrical Wedge Entering Water
'a -a
=0.02
0.04
-LO
y Vt
Figure 4b - Wedge Angle c1
+ c2
= 0.1 Radian0.06J
L... -0.2 -0.4 -0.6 -0.8 P V2P - V2 0.30
005
+ a1 0.2 RAD 0 -0.2 -0.4 -0.6 -0.B -1.0y/vf
Figure 5a - Wedge Angle c + = 0.2 Radian
=0.1 rad
0.2
0.4Figure Sb - Wedge Angle + a2 0.1 adiafl
Figure 5 - Pressure Distribution on the Suction
0.6 y Vt 0.05 P pV2 0 0.05
P
aV2 3
2 o-02
(SYMMETRICAL WEDGE) -0.8 -IO y/vtFigure 6 - Effect of Changing Angle on Pressure Distribution on the Pressure
Side of a Nonsymmetrical Wedge
VENTED FLAT PLATE
SYMMETRICAL WEDGE
I
I
Figure 7 - Pressure Distribution on a Vented
Flat Plate Entering a Water Surface
o -0.2 -0.4 P 2 -0.6 -0.8 -1.0 yi Vt
D
C-
D1
V2Vt
2 L CL = _pV2Vt , ,/
,
a12=O.2ra/
,
/ /T
/ /I,
NON SY MME TR IC AL WEDGE 0L FØ2 rod V F4T IL AT ING/
FLAT PLATE/
I I I 0.04 008 012 0.16 0.2 a, a2 - ø I rodFigure 8 - Drag and Lift
Coefficients of
Nonsymmetrical Wedges and
Ventilated
Flat Plates Entering Water
3. o -0.2 -0.4
îvet
-0.6-08
-.
X y,C+VtJC-IFigure 9 - Pressure Distribution on
Base-Vented
Thin Wedge Entering the Water at Fr
- Lo
6. 4. 2. 1,-P apV2
3.0 2.5-D calVIP 2.0 2 '.5 -0.8 I I 2 3 4
Vt/c
Vt 2aFigure 10 - Drag Coefficient of a Base-Vented Symmetrical Wedge Entering the Water with
Ventilation y Vt -1.0 -0.8 -06 -0.4 -0.2 0 0.2 04 0.6 0.8 1.0
/
/
/
/
--0.2II
/
/
/
--0.4/
/
/
/
/
--0.6/
/
/
/
/
/
/
-1.0Figure 11 - Cavity Shape of a Ventilated
Flat Plate Entering Water
X
Vt.
2.0 irD ZaZCPV! I .5 1.0REFERENCES
Yim, B., "An Application of Linearized Theory to Water Entry and Water Exit Problem Part i (with Cavity Effect)," NSRDC Report 3041 May
1969)
Tulin, M.P.., "Steady Two-Dirnen:ional Cavity Flows about Slender
BodiLs" David Taylor Mdel Basin Report 8.4 (May 1953).
. Cheng, H.K. and Rott, N., "Generalization of the Inversion
Formula of Thin Airfoil Theory," Journal of Rational Mechanics and
Analysis, Vol. 3, No. 3 (May 1954).
Milne-Thomson, L.M., "Theoretical Hydrodynamics," Fifth Edition,
The MacMillan Company, New York (1968).
Tulin, M.P., "Supercavitating Flows - Small Perturbation Theory,"
Journal of Ship Research, Vol. 7, p.o. 3 (Jan 1964).
Yim, B., "On a Fully Cavitating Two-Dimensional Flat Plate Hydrofoil with Non-Zero Cavitation Number Near a Free Surface," Hydro-nautics Incorporated Technical Report 463-4 (Jun 1964).
Moran, J.P., "The Vertical Water-Exit and Entry of Slender Symmetric Bodies," Journal of the Aerospace Science, Vol. 28, No. 10
1 Willi'm H. Mueller,
2 JSESPO Grumman Aircraft Engr Corp
1 J. Cuthbert Bethpage, Long Island,
1 A. Skolnick New York
Copies Copies
6 NAVSHIPSYSCOM 1 CIT, Prof T.Y. Wu
2 SHIPS 2021 2 MIT, Dept of Naval
1 PMS 383 Architecture
2 SHIPS 2052 i Prof J.N. Newman
1 SHIPS 034 i Prof L. Trilling,
6 NAVSEC Dept of Aeronaut Eng
i SEC 6000 2 Hydronautics, Inc
1 SEC 6103 1 M.P. Tulin
i SEC 6140 i P. Eisenberg
i SEC 6161
i SEC 6101 i Dr. H.N. Abrajnson,
1 SEC 6114E (Robert S. Director SWRI
Johnson) Dept Mechanical Sci
8500 Culebra Rd,
2 CHONR (Codes 438 E 463) San Antonio, Texas
2 NAVMAT (MAT 0331) 78206
Dir, ORL 1 Prof J.P. Moran
Graduate School of
USCG Attention: Sec, Ship
Struc Comm
Aerospace Engineering Cornell Univ,
Dir, BUSTAND, Fluid Ithaca, N.Y.
Mech Div
i
4
NASA
Copy to each lab.
3
Univ
of Calif., Berkeley, Calif., Dept of Eng1 Prof J. Wehausen i Prof M. Holt 1 Prof S. Berger
3 Institute of Mathematical Sci,
New York Univ 1 Prof J.J. Stoker 1 Prof P.R. Garabedian 1 Prof F. John i DIR, NRL INITIAL DISTRIBUTION General Electric Co Missile Space Div
King of Prussia, Pa. Dr. Andrew G. Fabula Naval Undersea Warfare Center 3203 E. Foothill Blvd Pasadena 8, Calif. 20 DDC
Commander, NWL Therm Advanced
NUL Research, Inc. 1 1 Code
Code
320, 322, Dr. Dr. A.E. Seigel A. May 100 Hudson Circle, Ithaca, N.Y. i 1 Code Code 702, 730, Dr. Lib G. Stathopoulos J.P.D.Wilkinson,
Consulting EngrUNCLASSIFIED
Security Classification
DOCUMENT CONTROL DATA - R & D
Security classification of title, body of abstract arid indexing annotation niust be entered when tine overall report is classified) ORIGINATING ACTIVITY (Corporate author)
Naval Ship Research E1 Development Center
Washington, D.C. 20034
20. REPORT SECURITY CLASSIPICATION
UNCLASSIFIED 2b. CROUP
3 REPORT TITLE
AN APPLICATION OF LINEARIZED THEORY TO WATER ENTRY AND WATER EXIT PROBLEM
PART 2 (WITH VENTILATION)
4 DESCRIPTIVE NOTES (Type of report and inclusive dates) S AU THORISI (Fitsl natrne, middle initial, last name)
Bohyun Yim
B REPORT DATE
July 1970
70. TOTAL NO. OF PACES
33
7h. NO. OF REPS Ba. CONTRACT OR GRANT NO.
b. PROJECT NO SR 009 0101
s. d.
98. ORIGINATORS REPORT NUMBER(S)
3171
Sb. OTI-IER REPORT NO(S) (Any other numbers that may be assigned
this report)
5 DISTRIBUTION STATEMENT
This document has been approved for public release and sale; its distribution
is unlimited.
II. SUPPLEMENTARY NOTES 12 SPONSORING MILITARY ACTIVITY
Naval Ship Research E1 Development Center
General Hydromechanics Research Program
13 ABSTRACT
A conformal mapping technique is used to analyze two-dimensional thin foils entering a water surface vertically with ventilations. Boundary conditions are linearized, and
the gravity effect is neglected. Flow fields, pressure
dis-tributions, and drags are given in closed forms for an in-finite nonsymmetrical wedge, an inin-finite flat plate with ventilation from the leading edge, and a finite base-vented
UNCLASSTFT PD Security Classification
FORM 4473
4
KEY WORDS LINR A LINK B LINK C
ROLE w-r ROLE W ROLE WT
Water entry of flat plates Ventilation
Nonsymmetrical wedge
Pressure
D rag