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Volumn 3, Issue , 2006, Pages 1852-1860

Flight test measurements of surface pressure on unmanned scaled supersonic experimental airplane

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; PRESSURE DISTRIBUTION; PRESSURE MEASUREMENT; SUPERSONIC FLOW;

EID: 33845453330     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3483     Document Type: Conference Paper
Times cited : (13)

References (15)
  • 1
    • 85088758520 scopus 로고    scopus 로고
    • Supersonic experimental airplane (NEXST) for next generation SST technology - Development and flight test plane for the unmanned scaled supersonic glider
    • Reno, Jan.
    • Sakata, K., "Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology - Development and Flight Test Plane for the Unmanned Scaled Supersonic Glider-", AIAA Paper 2002-0527, Reno, Jan. 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.527
    • Sakata, K.1
  • 2
    • 84893456381 scopus 로고    scopus 로고
    • Aerodynamic design of unmanned and scaled supersonic experimental airplane in Japan
    • Finland, Jul.
    • Yoshida, K. and Makino, Y., "Aerodynamic Design of Unmanned and Scaled Supersonic Experimental Airplane in Japan," ECCOMAS 2004, Finland, Jul. 2004.
    • (2004) ECCOMAS 2004
    • Yoshida, K.1    Makino, Y.2
  • 3
    • 33845401624 scopus 로고    scopus 로고
    • Woomera test range and the launch of the NEXST-1 supersonic flight trial experiment
    • North America, Nov.
    • Nikoloff, P. and Onuki, T., "Woomera Test Range and the Launch of the NEXST-1 Supersonic Flight Trial Experiment," Aerospace Testing Expo 2005, North America, Nov. 2005.
    • (2005) Aerospace Testing Expo 2005
    • Nikoloff, P.1    Onuki, T.2
  • 5
    • 0004543345 scopus 로고
    • Numerical method for the design and analysis of wings at supersonic speed
    • Carlson, H. W. and Miller, D. S., "Numerical Method for the Design and Analysis of Wings at Supersonic Speed", NASA TND-7713, 1974.
    • (1974) NASA TND-7713
    • Carlson, H.W.1    Miller, D.S.2
  • 8
    • 0003897926 scopus 로고
    • Boundary layer transition predictions based on linear theory
    • Arnal, D., "Boundary Layer Transition Predictions Based on Linear Theory", AGARD Report No.793, 1993.
    • (1993) AGARD Report No.793
    • Arnal, D.1
  • 10
    • 0036872379 scopus 로고    scopus 로고
    • Transition measurement on the natural laminar flow wing at mach 2
    • Sugiura, H., Yoshida, K., Tokugawa, N., Takagi, S. and Nishizawa, A., "Transition Measurement on the Natural Laminar Flow Wing at Mach 2", Journal of Aircraft, Vol.39, No.6, pp.996-1002, 2002.
    • (2002) Journal of Aircraft , vol.39 , Issue.6 , pp. 996-1002
    • Sugiura, H.1    Yoshida, K.2    Tokugawa, N.3    Takagi, S.4    Nishizawa, A.5
  • 13
    • 33845385113 scopus 로고    scopus 로고
    • Aeroelastic analysis of the non-powered supersonic experimental airplane
    • Nagano, Oct. (in Japanese)
    • Kawakami, H., Kurotaki, T., Takatoya, T., Ueda, Y. and Kuroda, F., "Aeroelastic Analysis of the Non-powered Supersonic Experimental Airplane", 41st Aircraft Symposium, Nagano, Oct. 2003 (in Japanese).
    • (2003) 41st Aircraft Symposium
    • Kawakami, H.1    Kurotaki, T.2    Takatoya, T.3    Ueda, Y.4    Kuroda, F.5
  • 15
    • 33845411643 scopus 로고    scopus 로고
    • Transition detection on supersonic natural laminar flow wing in the
    • Tokugawa, N. and Yoshida, K., "Transition Detection on Supersonic Natural Laminar Flow Wing in the", AIAA Paper 2006-3165, 2006.
    • (2006) AIAA Paper , vol.2006 , Issue.3165
    • Tokugawa, N.1    Yoshida, K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.