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Volumn 35, Issue 5, 1998, Pages 626-632

Physics of resonance in a supersonic forward-facing cavity

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; FLIGHT DYNAMICS; HEAT TRANSFER; LASER APPLICATIONS; NATURAL FREQUENCIES; NOSE CONES; OSCILLATIONS; PRESSURE TRANSDUCERS; WIND TUNNELS;

EID: 0032156788     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3395     Document Type: Article
Times cited : (49)

References (31)
  • 1
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    • 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 scopus 로고
    • 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
  • 5
    • 0029306280 scopus 로고
    • 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
  • 8
    • 0001467422 scopus 로고
    • 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
  • 10
    • 3843090546 scopus 로고
    • 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
  • 18
    • 0000406298 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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 scopus 로고
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.