-
2
-
-
0642268488
-
Shock-shock interaction on a slender supersonic cone
-
BLANKENSHIP, V. D. 1964 Shock-shock interaction on a slender supersonic cone. J. Fluid Mech. 22, 599-615.
-
(1964)
J. Fluid Mech.
, vol.22
, pp. 599-615
-
-
Blankenship, V.D.1
-
3
-
-
25044436450
-
Experiments on the head-on shock-shock interaction
-
BROWN, E. A. & MULLANEY, G. J. 1965 Experiments on the head-on shock-shock interaction. AIAA J. 3, 2168-2170.
-
(1965)
AIAA J.
, vol.3
, pp. 2168-2170
-
-
Brown, E.A.1
Mullaney, G.J.2
-
5
-
-
0642299171
-
Shock-shock interaction studies for weak incident shocks
-
Picatinny Arsenal, NJ, USA
-
HUDGINS, H. E. & FRIEDMAN, E. M. 1973 Shock-shock interaction studies for weak incident shocks. TR-4590. Picatinny Arsenal, NJ, USA.
-
(1973)
TR-4590
-
-
Hudgins, H.E.1
Friedman, E.M.2
-
6
-
-
85007677010
-
Blast wave impingement on the slender wedge moving at hypersonic speeds
-
INGER, G. R. 1966 Blast wave impingement on the slender wedge moving at hypersonic speeds. AIAA J. 4, 428-435.
-
(1966)
AIAA J.
, vol.4
, pp. 428-435
-
-
Inger, G.R.1
-
7
-
-
0016558636
-
Three-dimensional shock-on-shock interaction problem
-
KUTLER, P. & SAKELL, L. 1976 Three-dimensional shock-on-shock interaction problem. AIAA J. 13, 1360-1367.
-
(1976)
AIAA J.
, vol.13
, pp. 1360-1367
-
-
Kutler, P.1
Sakell, L.2
-
8
-
-
0016485222
-
Two-dimensional shock-on-shock interaction problem
-
KUTLER, P., SAKELL, L. & AIELLO, G. 1975 Two-dimensional shock-on-shock interaction problem. AIAA J. 13, 361-367.
-
(1975)
AIAA J.
, vol.13
, pp. 361-367
-
-
Kutler, P.1
Sakell, L.2
Aiello, G.3
-
9
-
-
0642360428
-
A computerized model to predict the transient pressure distribution due to shock-shock interaction
-
LAGOW, J. & MURAD, P. 1975 A computerized model to predict the transient pressure distribution due to shock-shock interaction. Martin-Marietta Aerospace, Orlando, FL, USA.
-
(1975)
Martin-Marietta Aerospace, Orlando, FL, USA
-
-
Lagow, J.1
Murad, P.2
-
10
-
-
0010539849
-
Reconsideration of the shock-shock relations for the case of a non-quiescent gas ahead of the shock and verification with experiments
-
LI, H. & BEN-DOR, G. 1995 Reconsideration of the shock-shock relations for the case of a non-quiescent gas ahead of the shock and verification with experiments. Proc. R. Soc. Lond. A 451, 383-397.
-
(1995)
Proc. R. Soc. Lond. A
, vol.451
, pp. 383-397
-
-
Li, H.1
Ben-Dor, G.2
-
11
-
-
0028534396
-
Analytical prediction of the reflected-diffracted shock wave shape in the interaction of a regular reflection with an expansive corner
-
LI, H., BEN-DOR, G. & HAN, Z. Y. 1994 Analytical prediction of the reflected-diffracted shock wave shape in the interaction of a regular reflection with an expansive corner. Fluid Dyn. Res. 14, 229-239.
-
(1994)
Fluid Dyn. Res.
, vol.14
, pp. 229-239
-
-
Li, H.1
Ben-Dor, G.2
Han, Z.Y.3
-
12
-
-
0642360429
-
Study of blast-bow wave interaction in a wind tunnel
-
MERRITT, D. L. & ARONSON, P. M. 1965 Study of blast-bow wave interaction in a wind tunnel. AIAA Paper 65-5.
-
(1965)
AIAA Paper 65-5
-
-
Merritt, D.L.1
Aronson, P.M.2
-
13
-
-
0642268487
-
Wind tunnel simulation of head-on bow wave-blast wave interaction
-
Naval Ordnance Lab, White Oak, Maryland, USA
-
MERRITT, D. L. & ARONSON, P. M. 1967 Wind tunnel simulation of head-on bow wave-blast wave interaction. NOLTR 67-123. Naval Ordnance Lab, White Oak, Maryland, USA.
-
(1967)
NOLTR 67-123
-
-
Merritt, D.L.1
Aronson, P.M.2
-
14
-
-
0642299168
-
A note on shock-shock diffraction
-
MILES, J. W. 1965 A note on shock-shock diffraction. J. Fluid Mech. 22, 95-102.
-
(1965)
J. Fluid Mech.
, vol.22
, pp. 95-102
-
-
Miles, J.W.1
-
15
-
-
0642299169
-
Computer program for the calculation of the interaction of the blast wave with a non-uniform shock layer
-
MIT, Cambridge, MA, USA
-
MILLER, W. D., SCHINDEL, L. & RUETENIK, J. R. 1964 Computer program for the calculation of the interaction of the blast wave with a non-uniform shock layer. MIT Rep. ASRL-TR-121-2. MIT, Cambridge, MA, USA.
-
(1964)
MIT Rep. ASRL-TR-121-2
-
-
Miller, W.D.1
Schindel, L.2
Ruetenik, J.R.3
-
16
-
-
0004229559
-
Oblique reflection of shock
-
Navy Dept., Bureau of Ordinance, Washington, DC, USA
-
NEUMANN, J. VON 1943 Oblique reflection of shock. Explos. Res. Rep. 12. Navy Dept., Bureau of Ordinance, Washington, DC, USA (also Collected Works, Vol. 6, pp. 238-299, Pergamon).
-
(1943)
Explos. Res. Rep. 12
-
-
Von Neumann, J.1
-
17
-
-
0011626511
-
-
Pergamon
-
NEUMANN, J. VON 1943 Oblique reflection of shock. Explos. Res. Rep. 12. Navy Dept., Bureau of Ordinance, Washington, DC, USA (also Collected Works, Vol. 6, pp. 238-299, Pergamon).
-
Collected Works
, vol.6
, pp. 238-299
-
-
-
18
-
-
0642360431
-
Shock-on-shock pressure measurements at Mach 5 from rocket-propelled sled tests, phase I: Lateral intercepts
-
Kaman Aerospace Corp., Bloomfield, CN, USA
-
RUETENIK, J. R., COLE, E. L. & JONES, R. E. 1973 Shock-on-shock pressure measurements at Mach 5 from rocket-propelled sled tests, phase I: lateral intercepts. KAMAN AviDyne Rep. KA TR-98. Kaman Aerospace Corp., Bloomfield, CN, USA.
-
(1973)
KAMAN AviDyne Rep. KA TR-98
-
-
Ruetenik, J.R.1
Cole, E.L.2
Jones, R.E.3
-
19
-
-
0642268486
-
The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speed
-
SMYRL, J. L. 1963 The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speed. J. Fluid Mech. 15, 223-240.
-
(1963)
J. Fluid Mech.
, vol.15
, pp. 223-240
-
-
Smyrl, J.L.1
|