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Volumn 1, Issue , 2006, Pages 546-557

Water tunnel velocimetry results for the 1303 UCAV configuration

Author keywords

[No Author keywords available]

Indexed keywords

BENCHMARKING; FLOW VISUALIZATION; LAMINAR FLOW; REYNOLDS NUMBER; VELOCITY MEASUREMENT; WIND TUNNELS;

EID: 33845419597     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2990     Document Type: Conference Paper
Times cited : (17)

References (12)
  • 1
    • 85081445371 scopus 로고    scopus 로고
    • Ph.D. Thesis, Caltech
    • Jeon, D. Ph.D. Thesis, Caltech, 2000.
    • (2000)
    • Jeon, D.1
  • 2
    • 0025792678 scopus 로고
    • Digital particle image velocimetry
    • Willert, C.E., and Gharib, M. "Digital Particle Image Velocimetry". Experiments in Fluids, Vol. 10, 1991, pp.181-193.
    • (1991) Experiments in Fluids , vol.10 , pp. 181-193
    • Willert, C.E.1    Gharib, M.2
  • 6
    • 7544242032 scopus 로고    scopus 로고
    • Visualized vortices on unmanned combat air vehicle planform: Effect of reynolds number
    • Sep/Oct
    • Elkhoury, M., and Rockwell, D. "Visualized Vortices on Unmanned Combat Air Vehicle Planform: Effect of Reynolds Number". AIAA Journal of Aircraft, Vol. 41, No. 5, Sep/Oct 2004, pp. 1244-1247.
    • (2004) AIAA Journal of Aircraft , vol.41 , Issue.5 , pp. 1244-1247
    • Elkhoury, M.1    Rockwell, D.2
  • 7
    • 0037273369 scopus 로고    scopus 로고
    • Leading edge vortex structure of nonslender delta wings and low reynolds number
    • Jan
    • OL, M. and Gharib, M., "Leading Edge Vortex Structure of Nonslender Delta Wings and Low Reynolds Number". AIAA Journal, Vol. 41, No. 1, Jan 2003, pp. 16-26.
    • (2003) AIAA Journal , vol.41 , Issue.1 , pp. 16-26
    • Ol, M.1    Gharib, M.2
  • 8
    • 29344448611 scopus 로고    scopus 로고
    • Low speed wind tunnel tests on the 1303 ucav concept
    • QinetiQ, Ltd., Farnborough, UK, March
    • Bruce, R. J., Mundell, A. R. G., "Low Speed Wind Tunnel Tests on the 1303 UCAV Concept", QinetiQ/FST/TR025502/1.0, QinetiQ, Ltd., Farnborough, UK, March 2003.
    • (2003) QinetiQ/FST/TR025502/1.0
    • Bruce, R.J.1    Mundell, A.R.G.2
  • 9
    • 85081443612 scopus 로고    scopus 로고
    • http://www.stratasys.com/sys_polyjet.html.
  • 12
    • 0029341383 scopus 로고
    • Flow developments above 50-deg sweep delta wings with different leading-edge profiles
    • Jul.-Aug.
    • Miau, J.J., Kuo, K.T., Liu, W.H., Hsieh, S.J., Chou, J.H. and Lin, C.K. "Flow Developments above 50-Deg Sweep Delta Wings with Different Leading-Edge Profiles." J. Aircraft, Vol. 32, No. 4, Jul.-Aug. 1995.
    • (1995) J. Aircraft , vol.32 , Issue.4
    • Miau, J.J.1    Kuo, K.T.2    Liu, W.H.3    Hsieh, S.J.4    Chou, J.H.5    Lin, C.K.6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.