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Volumn 2, Issue , 2005, Pages 1614-1628

Influence of instationary aerodynamics and trimming on the dynamics of an aeroelastic aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC AIRCRAFTS; COOPER-HARPER RATING; INSTATIONARY AERODYNAMICS; PILOT QUESTIONNAIRES;

EID: 29344439186     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (15)
  • 3
    • 0003273227 scopus 로고
    • The use of pilot rating in the evaluation of aircraft handling qualities
    • Cooper, G. and R. Harper Jr. (1989). The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities. NASA TN D-5153.
    • (1989) NASA TN , vol.D-5153
    • Cooper, G.1    Harper Jr., R.2
  • 5
    • 0009489777 scopus 로고
    • A Modern Course in Aeroelasticity (Third revised and enlarged ed.). Kluwer Academic Publishers
    • Dowell, E. (Ed.) (1995). A Modern Course in Aeroelasticity (Third revised and enlarged ed.), Volume 32 of Solid Mechanics and its Applications. Kluwer Academic Publishers.
    • (1995) Solid Mechanics and Its Applications , vol.32
    • Dowell, E.1
  • 6
    • 0015160179 scopus 로고
    • An approximate true damping solution of the flutter equation by determinant iteration
    • Hassig, H. (1971). An approximate true damping solution of the flutter equation by determinant iteration. Journal of Aircraft 5(11), 885-889.
    • (1971) Journal of Aircraft , vol.5 , Issue.11 , pp. 885-889
    • Hassig, H.1
  • 7
    • 0006448575 scopus 로고    scopus 로고
    • AIAA Education Series. American Institute of Aeronautics and Astronautics, Inc.
    • Hodgkinson, J. (1998). Aircraft Handling Qualities. AIAA Education Series. American Institute of Aeronautics and Astronautics, Inc.
    • (1998) Aircraft Handling Qualities
    • Hodgkinson, J.1
  • 10
    • 0026221217 scopus 로고
    • Numerical and literal aeroelastic-vehicle-model reduction for feedback control synthesis
    • Sept.-Oct.
    • Newman, B. and D. Schmidt (1991, Sept.-Oct.). Numerical and literal aeroelastic-vehicle-model reduction for feedback control synthesis. Journal of Guidance, Control and Dynamics 14(5), 943-953.
    • (1991) Journal of Guidance, Control and Dynamics , vol.14 , Issue.5 , pp. 943-953
    • Newman, B.1    Schmidt, D.2
  • 15
    • 0024019482 scopus 로고
    • Flight dynamics of aeroelastic vehicles
    • June.
    • Waszak, M. and D. Schmidt (1988, June). Flight dynamics of aeroelastic vehicles. Journal of Aircraft 25(6), 563-571.
    • (1988) Journal of Aircraft , vol.25 , Issue.6 , pp. 563-571
    • Waszak, M.1    Schmidt, D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.