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Volumn 2, Issue , 2006, Pages 913-927

Transition detection on supersonic natural laminar flow wing in the flight

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; LAMINAR FLOW; PRESSURE MEASUREMENT; PRESSURE TRANSDUCERS; SENSORS; SUPERSONIC AIRCRAFT;

EID: 33845411643     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3165     Document Type: Conference Paper
Times cited : (15)

References (17)
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    • Yoshida, K., and Makino, Y., "Aerodynamic Design of Unmanned and Scaled Supersonic Experimental Airplane in Japan," ECCOMAS 2004, Jyväskylä/Finland, July, 2004.
    • (2004) ECCOMAS 2004
    • Yoshida, K.1    Makino, Y.2
  • 2
    • 0004543345 scopus 로고
    • Numerical method fot the design and analysis of wings at supersonic speeds
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    • (1974) NASA TN , vol.D7713
    • Carlson, H.W.1    Miller, D.S.2
  • 5
    • 0003620791 scopus 로고    scopus 로고
    • Overview of NAL's program including the Aerodynamic design of the scaled supersonic airplane
    • held at the VKI
    • Yoshida K., "Overview of NAL's Program Including the Aerodynamic Design of the Scaled Supersonic Airplane," held at the VKI, RTO Educational Notes 4, 15.1-16, 1998.
    • (1998) RTO Educational Notes , vol.4
    • Yoshida, K.1
  • 6
    • 33845402555 scopus 로고
    • Taerodynamic design of a supersonic airplane wing - Application of the natural laminar flow concept to airfoil
    • January. (in Japanese)
    • Ogoshi, H., "Taerodynamic Design of a Supersonic Airplane Wing - Application of the Natural Laminar Flow Concept to Airfoil," Proceedings of the 47th Natural Congress of Theoretical & Applied Mechanics, January, 1988. (in Japanese)
    • (1988) Proceedings of the 47th Natural Congress of Theoretical & Applied Mechanics
    • Ogoshi, H.1
  • 8
    • 0342642601 scopus 로고
    • Boundary layer transition prediction based on linear theory
    • Arnal D., "Boundary Layer Transition Prediction based on Linear Theory," AGARD Report, No. 793, 1993.
    • (1993) AGARD Report , Issue.793
    • Arnal, D.1
  • 10
    • 84878470321 scopus 로고    scopus 로고
    • Three dimensional boundary layer transition analysis in supersonic flow using a Navier-Stokes code
    • on CD-ROM
    • Ueda. Y., Ishikawa, H., and Yoshida, K., "Three Dimensional Boundary Layer Transition Analysis in Supersonic Flow Using a Navier-Stokes Code," Proceedings of ICAS 2004-2.8.2, on CD-ROM, 2004.
    • (2004) Proceedings of ICAS 2004-2.8.2
    • Ueda, Y.1    Ishikawa, H.2    Yoshida, K.3
  • 11
    • 0036872379 scopus 로고    scopus 로고
    • Transition measurements on the natural laminar flow wing at mach 2
    • 1002
    • Sugiura, H., Yoshida, K., Tokugawa, N., Takagi, S., and Nishizawa, A., "Transition Measurements on the Natural Laminar Flow Wing at Mach 2," Journal of Aircraft, Vol. 39, No. 6, 2002, pp. 996, 1002.
    • (2002) Journal of Aircraft , vol.39 , Issue.6 , pp. 996
    • Sugiura, H.1    Yoshida, K.2    Tokugawa, N.3    Takagi, S.4    Nishizawa, A.5
  • 12
    • 85086612515 scopus 로고    scopus 로고
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  • 13
    • 33845453330 scopus 로고    scopus 로고
    • Flight test measurements of surface pressure on unmanned scaled supersonic experimental airplane
    • Kwak, D.-Y. and Yoshida, K., "Flight Test Measurements of Surface Pressure on Unmanned Scaled Supersonic Experimental Airplane," AIAA Paper 2006-3483, 2006.
    • (2006) AIAA Paper , vol.2006 , Issue.3483
    • Kwak, D.-Y.1    Yoshida, K.2
  • 14
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    • Surface pressure measurement system for the flight test on supersonic experimental airplane (NEXST-1)
    • 178 in Japanese
    • Kwak, D.-Y., Yoshida, K. and Noguchi, M., "Surface Pressure Measurement System for the Flight Test on Supersonic Experimental Airplane (NEXST-1)," Proceedings of the 37th JSASS Annual Meeting, 2006, pp.175, 178 (in Japanese).
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  • 15
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    • Comparison of wind tunnel transition and freestream disturbance measurements
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  • 16
    • 0016600519 scopus 로고
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    • (1975) Journal of Fluid Mechanics , vol.72 , Issue.4 , pp. 731
    • Nishioka, M.1    Iida, S.2    Ichikawa, Y.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.