메뉴 건너뛰기




Volumn 9, Issue 3, 2005, Pages 211-221

Tests of the JAPHAR dual mode ramjet engine

Author keywords

Dual mode ramjet; Hypersonic vehicle; JAPHAR; Scramjet; Supersonic combustion; Thermal throat

Indexed keywords

CALORIMETRY; COMBUSTION; COMBUSTION CHAMBERS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; HYPERSONIC AERODYNAMICS;

EID: 15844410962     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.01.007     Document Type: Article
Times cited : (33)

References (11)
  • 1
    • 84964452711 scopus 로고
    • Experimental investigation of angled injection in a compressible flow
    • July
    • D. Bayley, R. Hartfield, Experimental investigation of angled injection in a compressible flow, AIAA paper 95-2414, July 1995
    • (1995) AIAA Paper , vol.95 , Issue.2414
    • Bayley, D.1    Hartfield, R.2
  • 4
    • 1042270342 scopus 로고    scopus 로고
    • Weighing of the JAPHAR dual mode ramjet engine
    • Orléans, France
    • O. Dessornes, D. Scherrer, Weighing of the JAPHAR dual mode ramjet engine, AIAA paper 2002-5187, Orléans, France, 2002
    • (2002) AIAA Paper , vol.2002 , Issue.5187
    • Dessornes, O.1    Scherrer, D.2
  • 5
    • 15844364194 scopus 로고    scopus 로고
    • Testing and weighing of the japhar dual mode ramjet engine
    • Bengalore, India
    • O. Dessornes, D. Scherrer, P. Novelli, Testing and weighing of the japhar dual mode ramjet engine, ISABE paper 2001-1135, Bengalore, India
    • ISABE Paper , vol.2001 , Issue.1135
    • Dessornes, O.1    Scherrer, D.2    Novelli, P.3
  • 7
    • 15844390235 scopus 로고
    • Nozzle geometry effects on strut injection into a supersonic flow
    • September WL-TR-95-2143
    • D. Glawe, M. Samimy, A. Nejad, Nozzle geometry effects on strut injection into a supersonic flow, Wright laboratory final report, September 1995, WL-TR-95-2143
    • (1995) Wright Laboratory Final Report
    • Glawe, D.1    Samimy, M.2    Nejad, A.3
  • 8
    • 15844410883 scopus 로고    scopus 로고
    • An experimental investigation of transverse injection from circular and elliptical nozzles into a supersonic crossflow
    • January WL-TR-2102
    • M. Gruber, A. Nejad, J. Dutton, An experimental investigation of transverse injection from circular and elliptical nozzles into a supersonic crossflow, Wright laboratory final report, January 1996, WL-TR-2102
    • (1996) Wright Laboratory Final Report
    • Gruber, M.1    Nejad, A.2    Dutton, J.3
  • 9
    • 0023964290 scopus 로고
    • An analytical study of the hydrogen-air reaction mechanism with application to Scramjet combustion
    • February
    • C.J. Jachimowski, An analytical study of the hydrogen-air reaction mechanism with application to Scramjet Combustion, NASA technical paper 2791, February 1988
    • (1988) NASA Technical Paper , vol.2791
    • Jachimowski, C.J.1
  • 10
    • 15844415252 scopus 로고    scopus 로고
    • JAPHAR - A joint ONERA-DLR research project on high speed airbreathing propulsion, ISABE paper 99-7091
    • P. Novelli, and W. Koschel JAPHAR - A joint ONERA-DLR research project on high speed airbreathing propulsion, ISABE paper 99-7091 14th Symposium ISABE, Florence, Italy September 1999
    • (1999) 14th Symposium ISABE, Florence, Italy
    • Novelli, P.1    Koschel, W.2
  • 11
    • 15844391980 scopus 로고
    • Supersonic jet penetration (up to Mach 4) into a mach 2 Airstream
    • F. Povinelli, L.A. Povinelli, M. Hersch, Supersonic jet penetration (up to Mach 4) into a Mach 2 Airstream, AIAA paper 70-92, 1970
    • (1970) AIAA Paper , vol.70 , Issue.92
    • Povinelli, F.1    Povinelli, L.A.2    Hersch, M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.