메뉴 건너뛰기




Volumn , Issue , 2008, Pages

Physical modeling of aircraft upsets for real-time simulation applications

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ACCIDENTS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; LIFT; TABLE LOOKUP; TRAINING AIRCRAFT; VORTEX FLOW; WIND TUNNELS;

EID: 78651240461     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6205     Document Type: Conference Paper
Times cited : (6)

References (25)
  • 1
    • 27944460397 scopus 로고    scopus 로고
    • Federal Aviation Administration, available from, August
    • Federal Aviation Administration, "Airplane Upset Recovery Training Aid, Revision 1," available from http://www.faa.gov/avr/afs/afs200/afs210/ index.cfm, August 2004.
    • (2004) Airplane Upset Recovery Training Aid, Revision 1
  • 2
    • 19644371734 scopus 로고    scopus 로고
    • Statistical summary of commercial jet airplane accidents worldwide operations 1959-2005
    • Boeing Corporation, May
    • Boeing Corporation, "Statistical Summary of Commercial Jet Airplane Accidents Worldwide Operations 1959-2005," Aviation Safety, Boeing Commercial Airplanes, May 2006.
    • (2006) Aviation Safety, Boeing Commercial Airplanes
  • 8
    • 78651232946 scopus 로고    scopus 로고
    • available through, (note that a similarly titled article appeared in Air Line Pilot Magazine, January)
    • Wainwright, W., "Airplane Upset Recovery: A Test Pilot's View," available through http://www.skybrary.aero/bookshelf/content/index.php (note that a similarly titled article appeared in Air Line Pilot Magazine, January 2000).
    • (2000) Airplane Upset Recovery: A Test Pilot's View
    • Wainwright, W.1
  • 9
    • 85003340146 scopus 로고
    • Aerodynamic design features of the DC-9
    • November- December
    • Shevell, R.S. and Schaufele, R.D., "Aerodynamic Design Features of the DC-9," Journal of Aircraft, Vol. 3, (6), November- December 1966, pp. 515-523.
    • (1966) Journal of Aircraft , vol.3 , Issue.6 , pp. 515-523
    • Shevell, R.S.1    Schaufele, R.D.2
  • 11
    • 85069369672 scopus 로고
    • Reduction of stall-spin entry tendencies through wing aerodynamic design
    • April
    • Kroeger, R.A. and Feistel, T.W., "Reduction of Stall-Spin Entry Tendencies through Wing Aerodynamic Design," SAE Paper 760481, April 1976.
    • (1976) SAE Paper 760481
    • Kroeger, R.A.1    Feistel, T.W.2
  • 12
    • 0019265564 scopus 로고
    • Numerical lifting line theory applied to drooped leading edge wings below and above stall
    • December
    • Anderson, J.D., Corda, S., and Wie, D., "Numerical Lifting Line Theory Applied to Drooped Leading Edge Wings Below and Above Stall," Journal of Aircraft, Vol. 17, (12), December 1980, pp. 898-904.
    • (1980) Journal of Aircraft , vol.17 , Issue.12 , pp. 898-904
    • Anderson, J.D.1    Corda, S.2    Wie, D.3
  • 13
    • 85067318333 scopus 로고    scopus 로고
    • Analytical prediction of airplane aerodynamic characteristics for pre- and post-stall conditions
    • AIAA 2001-2442, presented at the, Anaheim, CA, June
    • Dixon, C.J., "Analytical Prediction of Airplane Aerodynamic Characteristics for Pre- and Post-Stall Conditions," AIAA 2001-2442, presented at the AIAA 19th Aerodynamics Conference, Anaheim, CA, June 2001.
    • (2001) th Aerodynamics Conference
    • Dixon, C.J.1
  • 16
    • 33646555249 scopus 로고    scopus 로고
    • Austin and goliath
    • August
    • Wise, J., "Austin and Goliath," Popular Science, Vol. 263, (2), August 2003.
    • (2003) Popular Science , vol.263 , Issue.2
    • Wise, J.1
  • 18
    • 0029272529 scopus 로고
    • Finite state induced flow models part II: Three-dimensional rotor disk
    • Peters, D. A. and He, C. J., "Finite State Induced Flow Models Part II: Three-Dimensional Rotor Disk," Journal of Aircraft, Vol. 32, (2), 1995, pp. 323-333.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 323-333
    • Peters, D.A.1    He, C.J.2
  • 21
    • 84888776508 scopus 로고    scopus 로고
    • High fidelity helicopter simulation using free wake, lifting line tail, and blade element tail rotor models
    • Phoenix, AZ
    • th Annual Forum, Phoenix, AZ, 2003.
    • (2003) th Annual Forum
    • Spoldi, S.1    Ruckel, P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.