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Volumn 2, Issue , 2004, Pages 1207-1223

Aerodynamic characteristics and glide-back performance of langley glide-back booster

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; BOOSTERS (ROCKET); CATAPULTS (AIRCRAFT LAUNCHERS); DATABASE SYSTEMS; OPTIMIZATION; ORBITS; SPEED; SUPERSONIC AIRCRAFT; WIND TUNNELS;

EID: 20544462275     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5382     Document Type: Conference Paper
Times cited : (20)

References (18)
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  • 5
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    • Journal of Spacecraft and Rockets , vol.38 , Issue.3 , pp. 334-344
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  • 7
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    • Description and calibration of the langley unitary plan wind tunnel
    • Nov.
    • Jackson, C.M., Corlett, W.A., and Monta, W.J.: Description and Calibration of the Langley Unitary Plan Wind Tunnel, NASA TP-1905, Nov. 1981.
    • (1981) NASA TP-1905
    • Jackson, C.M.1    Corlett, W.A.2    Monta, W.J.3
  • 8
    • 85067322174 scopus 로고    scopus 로고
    • Stage separation wind tunnel tests of a generic two-stage-to-orbit launch vehicle
    • July
    • Borderlon, W. J., Frost, A.L., and Reed, D, K.: Stage Separation Wind Tunnel Tests of a Generic Two-Stage-to-Orbit Launch Vehicle, AIAA Paper 2003-4227, July 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.4227
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  • 9
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    • Use of grit-type boundary-layer-transition trips on wind-tunnel models
    • Braslow, Albert I.; Hicks, Raymond M.; and Harris, Roy V., Jr.: Use of Grit-Type Boundary-Layer-Transition Trips on Wind-Tunnel Models. NASA TN D-3579, 1966.
    • (1966) NASA TN D-3579
    • Braslow, A.I.1    Hicks, R.M.2    Harris Jr., R.V.3
  • 10
    • 20544446520 scopus 로고
    • Effects of roughness size on the position of boundary-layer-transition and on the aerodynamic characteristics of a 55-degree swept delta wing at supersonic speeds
    • Stallings, Robert L., Jr.; and Lamb, Milton: Effects of Roughness size on the Position of Boundary-Layer-Transition and on the Aerodynamic Characteristics of a 55-degree Swept Delta Wing at Supersonic Speeds. NASA TP-1027, 1977.
    • (1977) NASA TP-1027
    • Stallings Jr., R.L.1    Lamb, M.2
  • 11
    • 20544439707 scopus 로고
    • Procedures and requirements for testing in the langley research center unitary plan wind tunnel
    • Wassum, Donald L.; and Hyman, Curtis E., Jr.: Procedures and Requirements for Testing in the Langley Research Center Unitary Plan Wind Tunnel. MASA TM-100529, 1988.
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    • Wassum, D.L.1    Hyman Jr., C.E.2
  • 12
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  • 13
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    • Sova, G. and Divan P.: Aerodynamic Preliminary Analysis System II, Part II- User's Manual, NASA CR-182077, April 1991.
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    • Sova, G.1    Divan, P.2
  • 14
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  • 15
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.