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Volumn , Issue , 2004, Pages

Ground testing of the hyshot supersonic combustion flight experiment in HEG and comparison with flight data

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; PROPULSION; RAMJET ENGINES; SUPERSONIC AERODYNAMICS; UNMANNED VEHICLES; WIND TUNNELS;

EID: 85086421980     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-3345     Document Type: Conference Paper
Times cited : (30)

References (7)
  • 1
    • 84956844821 scopus 로고
    • First results of the calibration and use of the HEG
    • AIAA 1994-2525, Colorado Springs, June 20-23
    • Eitelberg, G., First results of the calibration and use of the HEG, AIAA 1994-2525, 18th AIAA Aerospace Ground Testing Conference, Colorado Springs, June 20-23, 1994
    • (1994) 18th AIAA Aerospace Ground Testing Conference
    • Eitelberg, G.1
  • 4
    • 84894737316 scopus 로고    scopus 로고
    • High Enthalpy Flows in the HEG Shock Tunnel: Experiment and Numerical Rebuilding
    • AIAA 2003-0978, Reno, 6-9 January
    • Hannemann, K., High Enthalpy Flows in the HEG Shock Tunnel: Experiment and Numerical Rebuilding, AIAA 2003-0978, 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, 6-9 January, 2003
    • (2003) 41st AIAA Aerospace Sciences Meeting and Exhibit
    • Hannemann, K.1
  • 5
    • 0016494549 scopus 로고
    • Comparison of shock-induced two-and three-dimensional incipient turbulent separation
    • Korkegi, R.H., Comparison of shock-induced two-and three-dimensional incipient turbulent separation, AIAA journal, Vol 13, No 4, pp 534-535, 1975.
    • (1975) AIAA journal , vol.13 , Issue.4 , pp. 534-535
    • Korkegi, R.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.