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Volumn 43, Issue 2, 1998, Pages 110-119

A parametric design study for actively controlled trailing edge flaps

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; CONTROL SYSTEM ANALYSIS; MECHANICAL VARIABLES CONTROL;

EID: 0032045955     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.43.110     Document Type: Article
Times cited : (61)

References (19)
  • 1
    • 11744317427 scopus 로고    scopus 로고
    • "Screw Propeller of Helicopter Flying Machines," U.S. Patent 1,449,129, filed July 17, 1920, issued Mar 20, 1923
    • Pescara, R. P., "Screw Propeller of Helicopter Flying Machines," U.S. Patent 1,449,129, filed July 17, 1920, issued Mar 20, 1923.
    • Pescara, R.P.1
  • 5
    • 0031374435 scopus 로고    scopus 로고
    • Testing and Validation of a Froude scaled Helicopter Rotor model with Piezo-bimorph actuated Trailing Edge Flaps
    • San Diego, Mar
    • Koratkar, N. A. and Chopra, I. "Testing and Validation of a Froude scaled Helicopter Rotor model with Piezo-bimorph actuated Trailing Edge Flaps," Proceedings of the SPIE Smart Structures and Materials Symposium, San Diego, Mar 1997.
    • (1997) Proceedings of the SPIE Smart Structures and Materials Symposium
    • Koratkar, N.A.1    Chopra, I.2
  • 10
  • 14
    • 0012471984 scopus 로고
    • University of Maryland Advanced Rotor Code (UMARC) Theory Manual
    • Center for Rotorcraft Education and Research, University of Maryland, College Park, Maryland, Jul
    • Bir, G., Chopra, I., et al. "University of Maryland Advanced Rotor Code (UMARC) Theory Manual," Technical Report UM-AERO 94-18, Center for Rotorcraft Education and Research, University of Maryland, College Park, Maryland, Jul 1994.
    • (1994) Technical Report UM-AERO 94-18
    • Bir, G.1    Chopra, I.2
  • 19
    • 0005188729 scopus 로고
    • The Practical Implementation of an Actively Controlled Flap to Reduce Vibrations in Helicopter Rotors
    • St. Louis, May
    • Millott, T. A. and Friedmann, P. P. "The Practical Implementation of an Actively Controlled Flap to Reduce Vibrations in Helicopter Rotors," Proceedings of the 49th Annual Forum of the American Helicopter Society, pp. 1079-1092, St. Louis, May 1993.
    • (1993) Proceedings of the 49th Annual Forum of the American Helicopter Society , pp. 1079-1092
    • Millott, T.A.1    Friedmann, P.P.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.