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Volumn 1, Issue , 2006, Pages 438-454

Low speed wind tunnel tests on the 1303 UCAV concept

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; INTERNATIONAL COOPERATION; PRESSURE MEASUREMENT; REYNOLDS NUMBER; WIND TUNNELS; WINGS;

EID: 33845465821     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2985     Document Type: Conference Paper
Times cited : (46)

References (11)
  • 1
    • 5244333667 scopus 로고
    • A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds number
    • May
    • Furlong G. C. and McHugh J. G., "A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds number.", NACA Report 1339, May 1952.
    • (1952) NACA Report , vol.1339
    • Furlong, G.C.1    McHugh, J.G.2
  • 4
    • 85081451879 scopus 로고
    • Some notes on a visit to Edwards Air Force Base, California in May 1957
    • December
    • Andrews D. R., "Some notes on a visit to Edwards Air Force Base, California in May 1957.", RAE Tech Memo Aero 549, December 1957.
    • (1957) RAE Tech Memo Aero , vol.549
    • Andrews, D.R.1
  • 7
    • 85003242506 scopus 로고
    • A method for determining wall-interference corrections in solid-wall tunnels from measurements of static pressure at the walls
    • AGARD-CP-335
    • Ashill P. R. and Weeks D. J., "A method for determining wall-interference corrections in solid-wall tunnels from measurements of static pressure at the walls.", Wall Interference in Wind Tunnels, AGARD-CP-335, 1982.
    • (1982) Wall Interference in Wind Tunnels
    • Ashill, P.R.1    Weeks, D.J.2
  • 9
    • 33845382167 scopus 로고
    • Flow features of highly-swept wings at subsonic and supersonic speeds
    • September
    • Ashill P. R., Fulker J. L., Simmons M. J. and Betts C. J., "Flow features of highly-swept wings at subsonic and supersonic speeds.", ICAS-90-3.9.1, September 1990.
    • (1990) ICAS-90-3.9.1
    • Ashill, P.R.1    Fulker, J.L.2    Simmons, M.J.3    Betts, C.J.4
  • 10
    • 85081442383 scopus 로고
    • How the state of the boundary layer may affect the flow over slender wings
    • Smith J. H. B., "How the state of the boundary layer may affect the flow over slender wings.", RAE Tech Memo Aero 1157, 1969.
    • (1969) RAE Tech Memo Aero , vol.1157
    • Smith, J.H.B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.