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Volumn 25, Issue 3, 2009, Pages 417-419

Experimental demonstration of a new concept of drag reduction and thermal protection for hypersonic vehicles

Author keywords

Drag reduction; Hypersonic vehicle; Shock reconstruction; Spike and lateral jets; Thermal protection

Indexed keywords

ATTACK ANGLE; BLUNT BODIES; BOW SHOCKS; HYPERSONIC VEHICLE; HYPERSONIC VEHICLES; LATERAL JET; NEW CONCEPT; PEAK PRESSURE; PITCHING ANGLE; SHOCK-RECONSTRUCTION; SPIKE AND LATERAL JETS; THERMAL PROTECTION;

EID: 67651067960     PISSN: 05677718     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10409-009-0252-8     Document Type: Article
Times cited : (80)

References (5)
  • 3
    • 0024681585 scopus 로고
    • Forward facing spike effects of bodies of different cross section in supersonic flow
    • C.R. Hutt A.J. Howe 1989 Forward facing spike effects of bodies of different cross section in supersonic flow Aeronaut. J. R. Aeronaut. Soc. 93 6 229 234
    • (1989) Aeronaut. J. R. Aeronaut. Soc. , vol.93 , Issue.6 , pp. 229-234
    • Hutt, C.R.1    Howe, A.J.2
  • 5
    • 0142023856 scopus 로고    scopus 로고
    • Experimental investigations of hypersonic flow over highly blunted cones with aerospikes
    • V. Menezes S. Saravanan G. Jagadeesh K.P.J. Reddy 2003 Experimental investigations of hypersonic flow over highly blunted cones with aerospikes AIAA J. 41 10 1955 1961
    • (2003) AIAA J. , vol.41 , Issue.10 , pp. 1955-1961
    • Menezes, V.1    Saravanan, S.2    Jagadeesh, G.3    Reddy, K.P.J.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.