-
1
-
-
69649102379
-
-
BATCHELOR, G. K. 2000 An Introduction to Fluid Dynamics. Cambridge University Press.
-
BATCHELOR, G. K. 2000 An Introduction to Fluid Dynamics. Cambridge University Press.
-
-
-
-
2
-
-
0022013360
-
Modes of shock-wave oscillations on spike-tipped bodies
-
CALARESE, W. & HANKEY, W. L. 1985 Modes of shock-wave oscillations on spike-tipped bodies. AIAA J. 23, 185-192.
-
(1985)
AIAA J
, vol.23
, pp. 185-192
-
-
CALARESE, W.1
HANKEY, W.L.2
-
3
-
-
69649088922
-
-
CRAWFORD, D. H. 1959 Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8. NASA D-118.
-
CRAWFORD, D. H. 1959 Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8. NASA D-118.
-
-
-
-
6
-
-
0002876231
-
Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock
-
EDNEY, D. 1968 Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock. FFA Rep. 115.
-
(1968)
FFA Rep
, vol.115
-
-
EDNEY, D.1
-
7
-
-
0842290650
-
Driving mechanisms of high-speed unsteady spiked body flows. Part 1. Pulsation mode
-
FESZTY, D., BADCOCK, K. J. & RICHARDS, B. E. 2004a Driving mechanisms of high-speed unsteady spiked body flows. Part 1. Pulsation mode. AIAA J. 42, 95-106.
-
(2004)
AIAA J
, vol.42
, pp. 95-106
-
-
FESZTY, D.1
BADCOCK, K.J.2
RICHARDS, B.E.3
-
8
-
-
0842268988
-
Driving mechanisms of high-speed unsteady spiked body flows. Part 2. Oscillation mode
-
FESZTY, D., BADCOCK, K. J. & RICHARDS, B. E. 2004b 'Driving mechanisms of high-speed unsteady spiked body flows. Part 2. Oscillation mode. AIAA J. 42, 107-113.
-
(2004)
AIAA J
, vol.42
, pp. 107-113
-
-
FESZTY, D.1
BADCOCK, K.J.2
RICHARDS, B.E.3
-
9
-
-
0347838387
-
Comparisons between DSMC and Navier-Stokes solutions and measurements in regions of laminar shock wave boundary layer interaction in hypersonic flows
-
HOLDEN, M. S., WANDHAMS, T. P., HARVEY, J. K. & CANDLER, G. V. 2002 Comparisons between DSMC and Navier-Stokes solutions and measurements in regions of laminar shock wave boundary layer interaction in hypersonic flows. AIAA Paper 2002-0435.
-
(2002)
AIAA Paper
, pp. 2002-0435
-
-
HOLDEN, M.S.1
WANDHAMS, T.P.2
HARVEY, J.K.3
CANDLER, G.V.4
-
10
-
-
66949159971
-
Zur Stabilitaet geschlossener Grenzschichtabloese-gebiete an konischen Drenkoerpern bei Hyperschallaus-stroemung
-
KABELITZ, H. 1971 Zur Stabilitaet geschlossener Grenzschichtabloese-gebiete an konischen Drenkoerpern bei Hyperschallaus-stroemung. DLR FB 71-77.
-
(1971)
DLR FB
, pp. 71-77
-
-
KABELITZ, H.1
-
11
-
-
0006114497
-
-
Ph.D. Dissertation, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute And State University, Blacksburg, VA, USA
-
KENWORTHY, M. 1978 A study of unstable axisymmetric separation in high speed flows. Ph.D. Dissertation, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute And State University, Blacksburg, VA, USA.
-
(1978)
A study of unstable axisymmetric separation in high speed flows
-
-
KENWORTHY, M.1
-
12
-
-
0006835906
-
Experiments on separated boundary layers on probes in front of blunt nosed bodies in a supersonic air stream
-
MAIR, W. 1952 Experiments on separated boundary layers on probes in front of blunt nosed bodies in a supersonic air stream. Phil. Mag. 43, 695-716.
-
(1952)
Phil. Mag
, vol.43
, pp. 695-716
-
-
MAIR, W.1
-
13
-
-
69549156146
-
Hypersonic flow over axially symmetric spiked bodies
-
MAULL, D. 1962 Hypersonic flow over axially symmetric spiked bodies. J. Fluid Mech. 12, 614-624.
-
(1962)
J. Fluid Mech
, vol.12
, pp. 614-624
-
-
MAULL, D.1
-
14
-
-
0036258630
-
-
MEHTA, R. C. 2002 Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.80. Shock Waves 11 431-440.
-
MEHTA, R. C. 2002 Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.80. Shock Waves 11 431-440.
-
-
-
-
15
-
-
69649100895
-
-
MORRISON, J. H. 1992 A compressible Navier-Stokes solver with two-equation and Reynolds stress turbulence closure models. NASA CR-4440.
-
MORRISON, J. H. 1992 A compressible Navier-Stokes solver with two-equation and Reynolds stress turbulence closure models. NASA CR-4440.
-
-
-
-
16
-
-
69649092597
-
-
PANARAS, A. G. 1976 The high speed unsteady separation around concave bodies can be explained by an inviscid flow mechanism. These Annexe, VKI-Free University of Brussels.
-
PANARAS, A. G. 1976 The high speed unsteady separation around concave bodies can be explained by an inviscid flow mechanism. These Annexe, VKI-Free University of Brussels.
-
-
-
-
17
-
-
69649105926
-
-
PANARAS, A. G. 1977 High speed unsteady separation about concave bodies - A physical explanation, von Karman Institute, Tech. Note 123.
-
PANARAS, A. G. 1977 High speed unsteady separation about concave bodies - A physical explanation, von Karman Institute, Tech. Note 123.
-
-
-
-
18
-
-
85003322370
-
-
PANARAS A. G. 1981 Pulsating flows about axisymmetric concave bodies. AIAA J. 9, 804-806.
-
PANARAS A. G. 1981 Pulsating flows about axisymmetric concave bodies. AIAA J. 9, 804-806.
-
-
-
-
19
-
-
0022060741
-
-
PANARAS, A. G. 1985 Pressure pulses generated by the interaction of discrete vortices with an edge. J. Fluid Mech. 154, 445-462.
-
PANARAS, A. G. 1985 Pressure pulses generated by the interaction of discrete vortices with an edge. J. Fluid Mech. 154, 445-462.
-
-
-
-
20
-
-
2942757053
-
-
ROE, P. L. 1981 Approximate Riemann solvers, parameter vectors, and difference schemes. J. Comp. Phys. 43, 357-372.
-
ROE, P. L. 1981 Approximate Riemann solvers, parameter vectors, and difference schemes. J. Comp. Phys. 43, 357-372.
-
-
-
-
21
-
-
0030072022
-
Efficiency and accuracy of time-accurate turbulent Navier-Stokes computations
-
RUMSEY, C. L., SANETRIK, M. D., BIEDRON, R. T., MELSON, N. D. & PARLETTE, E. B. 1996 Efficiency and accuracy of time-accurate turbulent Navier-Stokes computations. Comput. Fluids. 25 (2), 217-236.
-
(1996)
Comput. Fluids
, vol.25
, Issue.2
, pp. 217-236
-
-
RUMSEY, C.L.1
SANETRIK, M.D.2
BIEDRON, R.T.3
MELSON, N.D.4
PARLETTE, E.B.5
-
22
-
-
69649097447
-
Shock boundary layer interaction in hypersonic high enthalpy flow on a double wedge
-
Paper 5150, Imperial College, London, UK, July 18-23
-
SCHRAMM, J. M. & EITELBERG, G 1999 Shock boundary layer interaction in hypersonic high enthalpy flow on a double wedge, Paper 5150, 22nd International Symposium on Shock Waves, Imperial College, London, UK, July 18-23.
-
(1999)
22nd International Symposium on Shock Waves
-
-
SCHRAMM, J.M.1
EITELBERG, G.2
-
23
-
-
69649084349
-
-
SHANG. J. S., HANKEY, W. L. & SMITH, R. E. 1980 Flow oscillations of spike-tipped bodies. AIAA Paper 80-0062.
-
SHANG. J. S., HANKEY, W. L. & SMITH, R. E. 1980 Flow oscillations of spike-tipped bodies. AIAA Paper 80-0062.
-
-
-
-
24
-
-
2442433925
-
Towards the ultimate conservative difference scheme V. A second order Sequel to Godunov's method
-
VAN LEER, B. 1979 Towards the ultimate conservative difference scheme V. A second order Sequel to Godunov's method. J. Comp. Phys. 32, 101-136.
-
(1979)
J. Comp. Phys
, vol.32
, pp. 101-136
-
-
VAN LEER, B.1
-
25
-
-
69649090896
-
Experimental flow over spiked flows
-
WOOD, C. 1960 Experimental flow over spiked flows. J. Fluid Mech. 8 584-594.
-
(1960)
J. Fluid Mech
, vol.8
, pp. 584-594
-
-
WOOD, C.1
-
26
-
-
69649097948
-
-
YEE, H. C. 2001 Building block for reliable non-linear numerical simulations. In Turbulent Flow Computation (Ed. D. Drikakis & B. Geurts). Kluwer Academic Publisher.
-
YEE, H. C. 2001 Building block for reliable non-linear numerical simulations. In Turbulent Flow Computation (Ed. D. Drikakis & B. Geurts). Kluwer Academic Publisher.
-
-
-
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