-
2
-
-
85006932445
-
-
Gasdynamik, Teubner, Stuttgart
-
Becker E (1965) Gasdynamik, Teubner, Stuttgart
-
(1965)
-
-
Becker, E.1
-
6
-
-
84962133639
-
Experimental verification of real gas effects in high enthalpy flows
-
Marseille, France
-
Eitelberg G (1993) Experimental verification of real gas effects in high enthalpy flows. Proc 19th ISSW, Marseille, France
-
(1993)
Proc 19Th ISSW
-
-
Eitelberg, G.1
-
8
-
-
85006910933
-
Transient pressure measurement at the end of a high enthalpy reflected shock tube
-
Bethlehem, Pa
-
Gourlay, C and R. Stalker (1989) Transient pressure measurement at the end of a high enthalpy reflected shock tube. Proc 17th ISSW, Bethlehem, Pa.
-
(1989)
Proc 17Th ISSW
-
-
Gourlay, C.1
Stalker, R.2
-
10
-
-
0344730398
-
Numerical simulation of reacting flows related to the HEG
-
Marseille
-
Hannemann K, Brenner G, Bruck S (1993) Numerical simulation of reacting flows related to the HEG. Proc. 19th ISSW, Marseille
-
(1993)
Proc. 19Th ISSW
-
-
Hannemann, K.1
Brenner, G.2
Bruck, S.3
-
12
-
-
84943741137
-
Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
-
Hornung HG (1972) Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders. J. Fluid Mech. 53, 149
-
(1972)
J. Fluid Mech
, vol.53
, pp. 149
-
-
Hornung, H.G.1
-
13
-
-
34347269932
-
Performance Data of the New Free‑Piston Shock Tunnel at GALC1T
-
Hornung HG (1992) Performance Data of the New Free‑Piston Shock Tunnel at GALC1T, AIAA 92-3943
-
(1992)
AIAA
, pp. 92-3943
-
-
Hornung, H.G.1
-
14
-
-
85006920832
-
-
Course given at CALCIT, Calif. Inst. of Technology, Pasadena
-
Hornung HG (1991) Class notes: Ae 234, Lecture Notes, Course given at CALCIT, Calif. Inst. of Technology, Pasadena
-
(1991)
Class Notes: Ae 234, Lecture Notes
-
-
Hornung, H.G.1
-
15
-
-
0041102137
-
Experimental Investigations of Shock Shock Interactions in the High Enthalpy Shock Tunnel Gottingen (HEG)
-
Marseille, France
-
Kortz S, McIntyre TJ, Eitelberg G (1993) Experimental Investigations of Shock Shock Interactions in the High Enthalpy Shock Tunnel Gottingen (HEG). Proc. 19th ISSW, Marseille, France
-
(1993)
Proc. 19Th ISSW
-
-
Kortz, S.1
McIntyre, T.J.2
Eitelberg, G.3
-
17
-
-
7244240848
-
-
DLR IB 1994.and report to Dassault Aviation
-
Krek R, Kasten D, Beck WH, Ueda S, EiteIberg G., Le Bozec A., (1994) Hermes Models 3036-2 and 3041 experiments in the HEG, DLR IB 1994.and report to Dassault Aviation
-
(1994)
Hermes Models 3036-2 and 3041 Experiments in the HEG
-
-
Krek, R.1
Kasten, D.2
Beck, W.H.3
Ueda, S.4
Eiteiberg, G.5
Le Bozec, A.6
-
21
-
-
84964195236
-
Comparison of the flow in the High Enthalpy Shock Tunnel in Gottingen with numerical simulations
-
Marseille, France
-
McIntyre TJ, Maus JR, Laster ML, Eitelberg G (1993) Comparison of the flow in the High Enthalpy Shock Tunnel in Gottingen with numerical simulations. Proc, 19th ISSW, Marseille, France
-
(1993)
Proc, 19Th ISSW
-
-
McIntyre, T.J.1
Maus, J.R.2
Laster, M.L.3
Eitelberg, G.4
-
22
-
-
85007684369
-
Shock tube test time limitation due to turbulent wall boundary layer
-
Mire's H (1964) Shock tube test time limitation due to turbulent wall boundary layer, AIAA Journal, Vol. 2, No 1.
-
(1964)
AIAA Journal
, vol.2
, Issue.1
-
-
Mire's, H.1
-
23
-
-
77958566917
-
-
NASA-CR-181721
-
Morgan, R.G., Paull, A., Stalker, R.J., Jacobs, P., Morris, N., Stringer, I. & Brescianini, C. (1989) Shock tunnel studies of scramjet phenomena, NASA-CR-181721.
-
(1989)
Shock Tunnel Studies of Scramjet Phenomena
-
-
Morgan, R.G.1
Paull, A.2
Stalker, R.J.3
Jacobs, P.4
Morris, N.5
Stringer, I.6
Brescianini, C.7
-
25
-
-
3643113312
-
An improved method to determine free stream conditions in hypersonic facilities
-
Olivier, H (1993) An improved method to determine free stream conditions in hypersonic facilities. Shock Waves, 2, 1993
-
(1993)
Shock Waves
, vol.2
, pp. 1993
-
-
Olivier, H.1
-
28
-
-
85006906455
-
Comparison of Computation and Experiment for a High Enthalpy, Heated-Driver, Shock-Tube Environment. AGARD Conf
-
Shahpar S, Kennaugh A, Hall IM, Poll A (1992) Comparison of Computation and Experiment for a High Enthalpy, Heated-Driver, Shock-Tube Environment. AGARD Conf. Proc. 514. Theoretical and Experimental Methods in Hypersonic Flows.
-
(1992)
Proc. 514. Theoretical and Experimental Methods in Hypersonic Flows
-
-
Shahpar, S.1
Kennaugh, A.2
Hall, I.M.3
Poll, A.4
-
29
-
-
0000616019
-
Development of a hypervelocity wind tunnel
-
Stalker RJ (1972) Development of a hypervelocity wind tunnel. J. Roy. Aeronautical Soc. 76 376-3M
-
(1972)
J. Roy. Aeronautical Soc
, vol.76
, pp. 43M-376
-
-
Stalker, R.J.1
|