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Volumn , Issue , 1996, Pages

Fluid dynamics of hypersonic forward-facing cavity flow

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; AMPLIFICATION; HYPERSONIC FLOW; MACH NUMBER; OSCILLATORS (ELECTRONIC);

EID: 84962184380     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (17)
  • 1
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    • (1990) High Velocity Impact Mechanics
    • Hohler, V.1    Stilp, A.J.2
  • 2
    • 0022964591 scopus 로고
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    • Hohler, V. and Stilp, A J. (1987): "Hypervelocity Penetration of Plate Targets by Rod-Like Projectiles," Int. J. Impact Engrg., Vol. 5, pp. 101-110.
    • (1987) Int. J. Impact Engrg. , vol.5 , pp. 101-110
    • Hohler, V.1    Stilp, A.J.2
  • 3
    • 67650988802 scopus 로고    scopus 로고
    • Nose-Tip Surface Heat Reduction Mechanism
    • Jan. 1996 (submitted to Thermophysics session)
    • Engblom, W.A., Goldstein, D.B., "Nose-Tip Surface Heat Reduction Mechanism," AIAA Paper 960354, Jan. 1996 (submitted to Thermophysics session).
    • AIAA Paper 960354
    • Engblom, W.A.1    Goldstein, D.B.2
  • 4
    • 19644381985 scopus 로고
    • On a New Method for the Generation of Sound Waves
    • Hartmann, J., and Troll B., "On a New Method for the Generation of Sound Waves," Phys. Rev., Vol. 20, 719-727,1922.
    • (1922) Phys. Rev. , vol.20 , pp. 719-727
    • Hartmann, J.1    Troll, B.2
  • 5
    • 3843139419 scopus 로고
    • Experiments Concerning the Hatrmann Whistle
    • UCLA Dept, of Engineering, Sep
    • Powell, A., and Smith, T.J., "Experiments Concerning the Hatrmann Whistle," Report 64-42, UCLA Dept, of Engineering, Sep. 1964.
    • (1964) Report 64-42
    • Powell, A.1    Smith, T.J.2
  • 9
    • 0027591763 scopus 로고
    • Mach 10 Bow- Shock Behavior of a Forward-Facing Nose Cavity
    • May-June
    • Huebner, L.D. and Utreja, L.R., "Mach 10 Bow- Shock Behavior of a Forward-Facing Nose Cavity," J. of Spacecraft and Rockets, Vol. 30, No. 3, May-June 1993.
    • (1993) J. of Spacecraft and Rockets , vol.30 , Issue.3
    • Huebner, L.D.1    Utreja, L.R.2
  • 11
    • 0029380030 scopus 로고
    • Computational Aeroacoustics: Issues and Methods
    • Jan
    • Tam, C.K.W., "Computational Aeroacoustics: Issues and Methods" AIAA Paper 95-0677, Jan 1995
    • (1995) AIAA Paper 95-0677
    • Tam, C.K.W.1
  • 12
    • 0029291727 scopus 로고
    • Quiet- Flow Ludwieg Tube for High-Speed Transition Research
    • Schneider, S.P., and Haven, C.E., 1995, "Quiet- Flow Ludwieg Tube for High-Speed Transition Research, " AIAA Journal, Vol.33, pp. 688-693.
    • (1995) AIAA Journal , vol.33 , pp. 688-693
    • Schneider, S.P.1    Haven, C.E.2
  • 14
    • 0000406298 scopus 로고
    • Aerothermodynamics in High-Speed Wind Tunnels at NASA Langley
    • Beckwith, I.E., and Miller, C.G., 1990, "Aerothermodynamics in High-Speed Wind Tunnels at NASA Langley," Annual Rev. Fluid Mech., Vol. 22, pp. 419-439.
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    • Beckwith, I.E.1    Miller, C.G.2
  • 17
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    • Effects of a Nose Cavity on Heat Transfer and Flowfield Over a Blunt Body at Mach 5
    • Jun
    • Yuceil, B. and Dolling, D.S., "Effects of a Nose Cavity on Heat Transfer and Flowfield Over a Blunt Body at Mach 5," AIAA Paper 94-2050, Jun. 1994.
    • (1994) AIAA Paper 94-2050
    • Yuceil, B.1    Dolling, D.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.