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Volumn , Issue , 2002, Pages

Experimental and computational, parametric drag study of an "Air Apike" in hypersonic flow

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL EFFORT; ELECTRICAL DISCHARGES; GASDYNAMIC EQUATIONS; LOW ENTHALPIES; PARAMETRIC STUDY; REDUCTION EFFECTS; STAGNATION PRESSURES; TEMPERATURE FLOW;

EID: 84896694017     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (24)
  • 1
    • 2942706505 scopus 로고
    • Exploratory studies of a Splked Body for Hypersonic Flight
    • Princeton University, Mar
    • Bogdonoff, S. M. and Vas, I. E. "Exploratory studies of a Splked Body for Hypersonic Flight, " Gas Dynamics Laboratory, Princeton University, Mar. 1958.
    • (1958) Gas Dynamics Laboratory
    • Bogdonoff, S.M.1    Vas, I.E.2
  • 2
    • 0013402201 scopus 로고    scopus 로고
    • 'Global Presence' Objective Drives Hypersonic Research
    • April 5
    • Covault, G. "'Global Presence' Objective Drives Hypersonic Research, " Aviation Week & Space Technology, April 5, 1999, pp. 54-58.
    • (1999) Aviation Week & Space Technology , pp. 54-58
    • Covault, G.1
  • 5
    • 33749161173 scopus 로고    scopus 로고
    • Experimental Investigation of the Hypersonic "Air Spike"
    • AIAA Paper 96-072 1, January
    • Marsh, J. J., Myrabo, L. N., Messitt, D. G., and Nagamatsu, H. T., "Experimental Investigation of the Hypersonic "Air Spike" Inlet at Mach IO, " AIAA Paper 96-072 1, January 1996.
    • (1996) Inlet at Mach IO
    • Marsh, J.J.1    Myrabo, L.N.2    Messitt, D.G.3    Nagamatsu, H.T.4
  • 9
    • 0027579904 scopus 로고
    • Hypersonic Shock-Tunnel Testing at an Equilibrium Interface Condition of 4100 K
    • Minucci, M. A. S., Nagamatsu, H. T., "Hypersonic Shock-Tunnel Testing at an Equilibrium Interface Condition of 4100 K, " Journal of Thermophysics and Heat Transfer, Vol. 7, No. 2, 1994, pp. 251-260.
    • (1994) Journal of Thermophysics and Heat Transfer , vol.7 , Issue.2 , pp. 251-260
    • Minucci, M.A.S.1    Nagamatsu, H.T.2
  • 10
    • 84894319056 scopus 로고    scopus 로고
    • The Flowfield of a Sonic Jet Exhausting against a Supersonic Flow
    • VI11 COBEM, Brazil, Dec. 1
    • Moraei-Jr., P. and Gamer, U. "The Flowfield of a Sonic Jet Exhausting against a Supersonic Flow, " VI11 COBEM, pp. 113-115, Brazil, Dec. 1.
    • Moraei Jr., P.1    Gamer, U.2
  • 13
    • 84889155929 scopus 로고
    • Laser Induced Air Spike for Advanced Transatmospheric Vehicles
    • AIAA-94-245 1, Colorado Springs, Co, June 20-23
    • Myrabo, L. N., and Raizer, Yu. P., "Laser Induced Air Spike for Advanced Transatmospheric Vehicles, " AIAA-94-245 1, 25th AIAA Plasmadynamics and Laser Conference, Colorado Springs, Co, June 20-23, 1994.
    • (1994) 25th AIAA Plasmadynamics and Laser Conference
    • Myrabo, L.N.1    Raizer, Y.P.2
  • 22
    • 85086489130 scopus 로고    scopus 로고
    • Experimental investigation of an electric arc Air-Spike with and without blunt body in hypersonic flow
    • AIAA paper 2001-0796, January, Reno, NV
    • Bracken R. M., Myrabo L. N., Nagamatsu H. T., Meloney E. D., Shneider M. N., Experimental investigation of an electric arc Air-Spike with and without blunt body in hypersonic flow, AIAA paper 2001-0796, 39th Aerospace Sciences Meeting&Exhibit, January 2001, Reno, NV.
    • (2001) 39th Aerospace Sciences Meeting&Exhibit
    • Bracken, R.M.1    Myrabo, L.N.2    Nagamatsu, H.T.3    Meloney, E.D.4    Shneider, M.N.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.