-
1
-
-
0027591763
-
Mach 10 Bow-Shock Behavior of a Forward-Facing Nose Cavity
-
Huebner, L. D., and Utreja, L. R., "Mach 10 Bow-Shock Behavior of a Forward-Facing Nose Cavity," Journal of Spacecraft and Rockets, Vol. 30, No. 3, 1993, pp. 291-297.
-
(1993)
Journal of Spacecraft and Rockets
, vol.30
, Issue.3
, pp. 291-297
-
-
Huebner, L.D.1
Utreja, L.R.2
-
2
-
-
0029386276
-
Nose Cavity Effects on Blunt Body Pressure and Temperatures at Mach 5
-
Yuceil, K. B., and Dolling, D. S., "Nose Cavity Effects on Blunt Body Pressure and Temperatures at Mach 5," Journal of Thermophysics and Heat Transfer, Vol. 9, No. 4, 1995, pp. 612-619.
-
(1995)
Journal of Thermophysics and Heat Transfer
, vol.9
, Issue.4
, pp. 612-619
-
-
Yuceil, K.B.1
Dolling, D.S.2
-
3
-
-
84997701840
-
-
AIAA Paper 92-2806, May
-
Shui, V., Reeves, B., and Thyson, N., "Multiple Aperture Window and Seeker Concepts for Endo KEW Applications," AIAA Paper 92-2806, May 1992.
-
(1992)
Multiple Aperture Window and Seeker Concepts for Endo KEW Applications
-
-
Shui, V.1
Reeves, B.2
Thyson, N.3
-
4
-
-
3843112257
-
-
AIAA Paper 95-0293. Jan.
-
Engblom, W. A., Yuceil, B., Goldstein, D. B., and Dolling, D. S., "Hypersonic Forward-Facing Cavity Flow: An Experimental and Numerical Study," AIAA Paper 95-0293. Jan. 1995.
-
(1995)
Hypersonic Forward-Facing Cavity Flow: An Experimental and Numerical Study
-
-
Engblom, W.A.1
Yuceil, B.2
Goldstein, D.B.3
Dolling, D.S.4
-
5
-
-
0029306280
-
Unsteady Flowfield over a Forward-Looking Endoatmospheric Hit-to-Kill Interceptor
-
Yang, H. Q., and Antonison, M., "Unsteady Flowfield over a Forward-Looking Endoatmospheric Hit-to-Kill Interceptor," Journal of Spacecraft and Rockets, Vol. 32, No. 3, 1995, pp. 440-444.
-
(1995)
Journal of Spacecraft and Rockets
, vol.32
, Issue.3
, pp. 440-444
-
-
Yang, H.Q.1
Antonison, M.2
-
7
-
-
3843139419
-
-
Dept. of Engineering, Rept. 64-42, Univ. of California, Los Angeles, CA, Sept.
-
Powell, A., and Smith, T. J., "Experiments Concerning the Hartmann Whistle," Dept. of Engineering, Rept. 64-42, Univ. of California, Los Angeles, CA, Sept. 1964.
-
(1964)
Experiments Concerning the Hartmann Whistle
-
-
Powell, A.1
Smith, T.J.2
-
8
-
-
0001467422
-
Experimental Investigation of Flow and Heating in a Resonance Tube
-
Sarohia, V., and Back, L. H., "Experimental Investigation of Flow and Heating in a Resonance Tube," Journal of Fluid Mechanics, Vol. 94, 1979, pp. 649-672.
-
(1979)
Journal of Fluid Mechanics
, vol.94
, pp. 649-672
-
-
Sarohia, V.1
Back, L.H.2
-
9
-
-
3843118791
-
-
Lockheed Missiles and Space Co., Inc., LMSC-D057194, April (NASA citation 76N25330)
-
Ericsson, L. E., and Reding, J. P., "Unsteady Aerodynamic Flow Field Analysis of the Space Shuttle Configuration. Part III: Unsteady Aerodynamics of Bodies with Concave Nose Geometries," Lockheed Missiles and Space Co., Inc., LMSC-D057194, April 1976 (NASA citation 76N25330).
-
(1976)
Unsteady Aerodynamic Flow Field Analysis of the Space Shuttle Configuration. Part III: Unsteady Aerodynamics of Bodies with Concave Nose Geometries
-
-
Ericsson, L.E.1
Reding, J.P.2
-
10
-
-
3843090546
-
-
Jet Propulsion Lab., California Inst. of Technology, TR 32-378, Pasadena, CA, July (NASA citation 63N13447)
-
Vrebalovich, T., "Resonance Tubes in a Supersonic Flow Field," Jet Propulsion Lab., California Inst. of Technology, TR 32-378, Pasadena, CA, July 1962 (NASA citation 63N13447).
-
(1962)
Resonance Tubes in a Supersonic Flow Field
-
-
Vrebalovich, T.1
-
13
-
-
84889209462
-
-
NASA TM-X-230, April
-
Smith, F. M., "A Wind-Tunnel Investigation of Effects of Nose Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90," NASA TM-X-230, April 1960.
-
(1960)
A Wind-Tunnel Investigation of Effects of Nose Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90
-
-
Smith, F.M.1
-
14
-
-
3843152744
-
-
AIAA Paper 87-2709, Oct.
-
Marquart, E. J., Grubb, J. B., and Utreja, L. R., "Bow-Shock Dynamics of a Forward-Facing Nose Cavity," AIAA Paper 87-2709, Oct. 1987.
-
(1987)
Bow-Shock Dynamics of a Forward-Facing Nose Cavity
-
-
Marquart, E.J.1
Grubb, J.B.2
Utreja, L.R.3
-
15
-
-
85072475157
-
-
Society of Automotive Engineers, Paper 871880, Warrendale, PA, Oct.
-
Huebner, L. D., and Utreja, L. R., "Experimental Flowfield Measurements of a Nose Cavity Configuration," Society of Automotive Engineers, Paper 871880, Warrendale, PA, Oct. 1987.
-
(1987)
Experimental Flowfield Measurements of a Nose Cavity Configuration
-
-
Huebner, L.D.1
Utreja, L.R.2
-
16
-
-
3843117710
-
-
AIAA Paper 87-1193, June
-
Sambamurthi, J. K., Huebner, L. D., and Utreja, L. R., "Hypersonic Flow Over a Cone with Nose Cavity," AIAA Paper 87-1193, June 1987.
-
(1987)
Hypersonic Flow over a Cone with Nose Cavity
-
-
Sambamurthi, J.K.1
Huebner, L.D.2
Utreja, L.R.3
-
18
-
-
0000406298
-
Aero-Thermodynamics in High-Speed Wind Tunnels at NASA Langley
-
Beckwith, I. E., and Miller, C. G., "Aero-Thermodynamics in High-Speed Wind Tunnels at NASA Langley," Annual Review of Fluid Mechanics, Vol. 22, 1990, pp. 419-439.
-
(1990)
Annual Review of Fluid Mechanics
, vol.22
, pp. 419-439
-
-
Beckwith, I.E.1
Miller, C.G.2
-
19
-
-
0029291727
-
Quiet-Flow Ludwieg Tube for High-Speed Transition Research
-
Schneider, S. P., and Haven, C. E., "Quiet-Flow Ludwieg Tube for High-Speed Transition Research," AIAA Journal, Vol. 33, No. 4, 1995, pp. 688-693.
-
(1995)
AIAA Journal
, vol.33
, Issue.4
, pp. 688-693
-
-
Schneider, S.P.1
Haven, C.E.2
-
20
-
-
0001763901
-
Aerodynamic Noise in Supersonic Wind Tunnels
-
Laufer, J., "Aerodynamic Noise in Supersonic Wind Tunnels," Journal of the Aerospace Sciences, Vol. 28, No. 9, 1961, pp. 685-692.
-
(1961)
Journal of the Aerospace Sciences
, vol.28
, Issue.9
, pp. 685-692
-
-
Laufer, J.1
-
21
-
-
85007654866
-
Radiated Aerodynamic Noise Effects on Boundary-Layer Transition in Supersonic and Hypersonic Wind Tunnels
-
Pate, S. R., and Schueler, C. J., "Radiated Aerodynamic Noise Effects on Boundary-Layer Transition in Supersonic and Hypersonic Wind Tunnels," AIAA Journal, Vol. 7, No. 3, 1969, pp. 450-457.
-
(1969)
AIAA Journal
, vol.7
, Issue.3
, pp. 450-457
-
-
Pate, S.R.1
Schueler, C.J.2
-
23
-
-
3843060204
-
-
NACA RM-L58D25a, July
-
Cooper, M., Beckwith, I. E., Jones, J. J., and Gallagher, J. J., "Heat-Transfer Measurements on a Concave Nose Shape with Unsteady-Flow Effects at Mach Numbers of 1.98 and 4.95," NACA RM-L58D25a, July 1958.
-
(1958)
Heat-Transfer Measurements on a Concave Nose Shape with Unsteady-Flow Effects at Mach Numbers of 1.98 and 4.95
-
-
Cooper, M.1
Beckwith, I.E.2
Jones, J.J.3
Gallagher, J.J.4
-
24
-
-
0031191830
-
Fluid Dynamics of Hypersonic Forward-Facing Cavity Flow
-
Engblom, W. A., Goldstein, D. B., Ladoon, D., and Schneider, S. P., "Fluid Dynamics of Hypersonic Forward-Facing Cavity Flow," Journal of Spacecraft and Rockets, Vol. 34, No. 4, 1997, pp. 437-444.
-
(1997)
Journal of Spacecraft and Rockets
, vol.34
, Issue.4
, pp. 437-444
-
-
Engblom, W.A.1
Goldstein, D.B.2
Ladoon, D.3
Schneider, S.P.4
-
25
-
-
0343018557
-
-
AIAA Paper 96-2191, June
-
Schneider, S. P., Collicott, S. H., Schmisseur, J. D., Ladoon, D., Randall, L. A., Munro, T. R., and Salyer, T. R.,"Laminar-Turbulent Transition Research in the Purdue Quiet-Flow Ludwieg Tube," AIAA Paper 96-2191, June 1996.
-
(1996)
Laminar-Turbulent Transition Research in the Purdue Quiet-Flow Ludwieg Tube
-
-
Schneider, S.P.1
Collicott, S.H.2
Schmisseur, J.D.3
Ladoon, D.4
Randall, L.A.5
Munro, T.R.6
Salyer, T.R.7
-
26
-
-
0010112786
-
-
Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, Dec.
-
Schmisseur, J. D.,"Receptivity of the Boundary Layer on a Mach-4 Elliptic Cone to Laser-Generated Localized Freestream Perturbations," Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue Univ., West Lafayette, IN, Dec. 1997.
-
(1997)
Receptivity of the Boundary Layer on a Mach-4 Elliptic Cone to Laser-Generated Localized Freestream Perturbations
-
-
Schmisseur, J.D.1
-
27
-
-
84983140525
-
-
AIAA Paper 98-0532, Jan.
-
Schmisseur, J. D., Schneider, S. P., and Collicott, S. H., "Receptivity of the Mach 4 Boundary Layer on an Elliptic Cone to Laser-Generated Localized Freestream Perturbations," AIAA Paper 98-0532, Jan. 1998.
-
(1998)
Receptivity of the Mach 4 Boundary Layer on An Elliptic Cone to Laser-Generated Localized Freestream Perturbations
-
-
Schmisseur, J.D.1
Schneider, S.P.2
Collicott, S.H.3
-
28
-
-
3843053544
-
-
AIAA Paper 97-0339, Jan.
-
Ladoon, D. W., Schmisseur, J. D., and Schneider, S. P.,"Laser-Induced Resonance in a Forward-Facing Cavity at Mach 4," AIAA Paper 97-0339, Jan. 1997.
-
(1997)
Laser-Induced Resonance in a Forward-Facing Cavity at Mach 4
-
-
Ladoon, D.W.1
Schmisseur, J.D.2
Schneider, S.P.3
-
30
-
-
0004208617
-
-
Wiley, New York
-
Liepmann, H. W., and Roshko, A., Elements of Gasdynamics, Wiley, New York, 1957.
-
(1957)
Elements of Gasdynamics
-
-
Liepmann, H.W.1
Roshko, A.2
-
31
-
-
0004098086
-
-
Wiley, New York
-
Kinsler, L. E., and Frey, A. R., Fundamentals of Acoustics, 2nd ed., Wiley, New York, 1962.
-
(1962)
Fundamentals of Acoustics, 2nd Ed.
-
-
Kinsler, L.E.1
Frey, A.R.2
|