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Volumn , Issue , 2008, Pages

Achievements obtained for sustained hypersonic flight within the LAPCAT project

Author keywords

[No Author keywords available]

Indexed keywords

AIR BREATHING ENGINES; BRUSSELS; COMBINED CYCLE; EUROPEAN COMMISSION; EXPERIMENTAL CAMPAIGN; FLIGHT REGIME; FUNDAMENTAL RESEARCH; HYPERSONIC FLIGHTS; MISSION REQUIREMENTS; NUMERICAL MODELLING; OPERATIONAL CONDITIONS; PROPULSION CONCEPT; RESEARCH AND DEVELOPMENT; RESEARCH INSTITUTIONS; VEHICLE SYSTEM;

EID: 68149084182     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (53)

References (14)
  • 4
    • 33947212863 scopus 로고    scopus 로고
    • Research on TBCC propulsion for a mach 4.5 supersonic cruise airliner
    • AIAA 2006-7976, 06-09 November
    • Sippel, M., Research on TBCC Propulsion for a Mach 4.5 Supersonic Cruise Airliner, 14th AIAA Int. Space Planes and Hypersonic Systems and Technologies, AIAA 2006-7976, 06-09 November 2006, Canberra, Australia.
    • (2006) th AIAA Int. Space Planes and Hypersonic Systems and Technologies
    • Sippel, M.1
  • 12
    • 77958512652 scopus 로고    scopus 로고
    • Effect of the turbulent schmit number on supersonic regime
    • 07-11/01, Reno (NV), USA
    • Ingenito A. and Bruno C., 'effect of the Turbulent schmit Number on Supersonic Regime', 46th AIAA Aerospace Sciences meeting and Exibit, 07-11/01 2008, Reno (NV), USA.
    • (2008) th AIAA Aerospace Sciences Meeting and Exibit
    • Ingenito, A.1    Bruno, C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.