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Volumn 40, Issue 3, 2002, Pages 481-489

Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surface

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CARBON DIOXIDE; ENTHALPY; NITROGEN; POROSITY; ULTRASONIC ABSORPTION;

EID: 0036493813     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1671     Document Type: Article
Times cited : (161)

References (25)
  • 11
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    • Performance data of the new free-piston Shock Tunnel T5 at GALCIT
    • July
    • (1992) AIAA Paper , vol.92 , Issue.3943
    • Hornung, H.G.1
  • 13
    • 0006058836 scopus 로고    scopus 로고
    • Boundary layer transition measurements in hypervelocity flows in a shock tunnel
    • Jan
    • (2001) AIAA Paper , vol.2001 , Issue.208
    • Mee, D.J.1
  • 24
    • 25744433178 scopus 로고    scopus 로고
    • Roughness-dominated transition on nosetips, attachment lines and lifting-entry vehicles
    • Jan
    • (2001) AIAA Paper , vol.2001 , Issue.205
    • Reda, D.C.1
  • 25
    • 85007654866 scopus 로고
    • Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels
    • (1969) AIAA Journal , vol.7 , Issue.2 , pp. 450-457
    • Pate, S.R.1    Schueler, C.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.