-
1
-
-
0015726428
-
Unsteady flow phenomena in shock tube nozzles
-
Bershader D; Griffith W (eds) Stanford Univ. Press, Stanford
-
Amann HO; Reichenbach H (1973) Unsteady flow phenomena in shock tube nozzles. In: Bershader D; Griffith W (eds) Recent developments in shock research. Stanford Univ. Press, Stanford, pp 96-112
-
(1973)
Recent Developments in Shock Research
, pp. 96-112
-
-
Amann, H.O.1
Reichenbach, H.2
-
2
-
-
0000104174
-
Thin layer approximation and algebraic model for separated turbulent flows
-
Baldwin BS; Lomax H (1978) Thin layer approximation and algebraic model for separated turbulent flows, AIAA Paper 78-257
-
(1978)
AIAA Paper 78-257
-
-
Baldwin, B.S.1
Lomax, H.2
-
3
-
-
24044431696
-
Numerical analysis of starting phase transients in a high enthalpy shock tunnel nozzle
-
Tokyo
-
Chue RSM (1996) Numerical analysis of starting phase transients in a high enthalpy shock tunnel nozzle. In: Proc Symp on Shock Waves, Japan '95, Tokyo
-
(1996)
Proc Symp on Shock Waves, Japan '95
-
-
Chue, R.S.M.1
-
4
-
-
36849097332
-
Influence of reflected shock and boundary-layer interaction on shock-tube flows
-
Davies L; Wilson JL (1969) Influence of reflected shock and boundary-layer interaction on shock-tube flows. Phys Fluids Suppl I: I-37-I-43
-
(1969)
Phys Fluids Suppl
, vol.1
-
-
Davies, L.1
Wilson, J.L.2
-
6
-
-
0001893517
-
A theoretical and experimental study of shock-tube flows
-
Glass II; Patterson GN (1955) A theoretical and experimental study of shock-tube flows. J Aeron Sci 22: 73-100
-
(1955)
J Aeron Sci
, vol.22
, pp. 73-100
-
-
Glass, I.I.1
Patterson, G.N.2
-
7
-
-
34347228415
-
Experimentai hypervelocity flow simulation, needs, achievements, and limitations
-
Tainan, Taiwan, 1993
-
Hornung H (1993) Experimentai hypervelocity flow simulation, needs, achievements, and limitations. Presented at the First Pacific Int Conf on Aerospace Science and Technology, Tainan, Taiwan, 1993
-
(1993)
First Pacific Int Conf on Aerospace Science and Technology
-
-
Hornung, H.1
-
9
-
-
85006932773
-
Transient, hypervelocity flow in an axisymmetric nozzle
-
Jacobs PA (1991) Transient, hypervelocity flow in an axisymmetric nozzle. AIAA Paper 91-0295
-
(1991)
AIAA Paper 91-0295
-
-
Jacobs, P.A.1
-
12
-
-
85007684369
-
Shock tube test time limitation due to turbulent-wall boundary layer
-
Mirels H (1964) Shock tube test time limitation due to turbulent-wall boundary layer. AIAA J 2: 38-54
-
(1964)
AIAA J
, vol.2
, pp. 38-54
-
-
Mirels, H.1
-
13
-
-
0001263787
-
The starting process in a hypersonic nozzle
-
Smith CE (1966) The starting process in a hypersonic nozzle. J Fluid Mech 24: 625-640
-
(1966)
J Fluid Mech
, vol.24
, pp. 625-640
-
-
Smith, C.E.1
-
14
-
-
85003325906
-
Driver gas contamination in a high-enthalpy reflected shock tunnel
-
Stalker RJ; Crane KCA (1978) Driver gas contamination in a high-enthalpy reflected shock tunnel. AIAA J 16: 277-279
-
(1978)
AIAA J
, vol.16
, pp. 277-279
-
-
Stalker, R.J.1
Crane, K.C.A.2
-
15
-
-
0007613491
-
Detection and reduction of driver gas contamination in a high-enthalpy shock tunnel
-
Sudani N; Hornung HG (1997) Detection and reduction of driver gas contamination in a high-enthalpy shock tunnel. In: Proc 21st Int. shock wave Symp Australia
-
(1997)
Proc 21st Int. Shock Wave Symp Australia
-
-
Sudani, N.1
Hornung, H.G.2
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