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Volumn II, Issue , 2006, Pages 1011-1021

Integrated trailing-edge flaps and servotabs for helicopter primary control

Author keywords

[No Author keywords available]

Indexed keywords

SERVOTABS; SWASHPLATELESS PRIMARY CONTROL SYSTEM; TRAILING-EDGE FLAPS; TRIM ANALYSIS;

EID: 33748475838     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (14)
  • 2
    • 0035389792 scopus 로고    scopus 로고
    • Aeroelastic analysis of rotors with trailing edge flaps using comprehensive codes
    • July
    • Straub, F. and Charles, B., "Aeroelastic Analysis of Rotors with Trailing Edge Flaps Using Comprehensive Codes," Journal of the American Helicopter Society, vol.46, no.3, July 2001, pp. 192-199.
    • (2001) Journal of the American Helicopter Society , vol.46 , Issue.3 , pp. 192-199
    • Straub, F.1    Charles, B.2
  • 3
    • 10944267141 scopus 로고    scopus 로고
    • Swashplateless helicopter rotor with trailing-edge flaps
    • November-December
    • Shen, Jinwei, and Chopra, I., "Swashplateless Helicopter Rotor with Trailing-Edge Flaps," Journal of Aircraft, vol.41, no.6, November-December 2004, pp. 1465-1472.
    • (2004) Journal of Aircraft , vol.41 , Issue.6 , pp. 1465-1472
    • Shen, J.1    Chopra, I.2
  • 5
    • 0035306701 scopus 로고    scopus 로고
    • Hover testing of a small-scale rotor with on-blade elevons
    • April
    • Fulton, M. and Ormiston, R., "Hover Testing of a Small-Scale Rotor with On-Blade Elevons," Journal of the American Helicopter Society, vol.46, no.2, April 2001, pp. 96-106.
    • (2001) Journal of the American Helicopter Society , vol.46 , Issue.2 , pp. 96-106
    • Fulton, M.1    Ormiston, R.2
  • 6
    • 0036802559 scopus 로고    scopus 로고
    • Wind tunnel testing of a smart rotor model with trailingedge flaps
    • October
    • Koratkar, N. and Chopra, I., "Wind Tunnel Testing of a Smart Rotor Model with Trailingedge Flaps," Journal of the American Helicopter Society, vol. 47, no.4, October 2002, pp. 263-272.
    • (2002) Journal of the American Helicopter Society , vol.47 , Issue.4 , pp. 263-272
    • Koratkar, N.1    Chopra, I.2
  • 7
    • 0043268211 scopus 로고    scopus 로고
    • Individual blade control methodology for a rotor with dissimilar blades
    • July
    • Roget, B. and Chopra, I., "Individual Blade Control Methodology for a Rotor with Dissimilar Blades," Journal of the American Helicopter Society, vol.48, no.3, July 2003, pp. 176-185.
    • (2003) Journal of the American Helicopter Society , vol.48 , Issue.3 , pp. 176-185
    • Roget, B.1    Chopra, I.2
  • 8
    • 14044252803 scopus 로고    scopus 로고
    • Experimental/numerical evaluation of integral trailing edge flaps for helicopter rotor applications
    • January
    • Hassan, A., Straub, F., and Noonan, K., "Experimental/Numerical Evaluation of Integral Trailing Edge Flaps for Helicopter Rotor Applications," Journal of the American Helicopter Society, vol.50, no.1, January 2005, pp. 3-17.
    • (2005) Journal of the American Helicopter Society , vol.50 , Issue.1 , pp. 3-17
    • Hassan, A.1    Straub, F.2    Noonan, K.3
  • 10
    • 0003866245 scopus 로고
    • Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance
    • Theodorsen, T. and Garrick, I.E., "Nonstationary Flow About a Wing-Aileron-Tab Combination Including Aerodynamic Balance," NACA Technical Report no. 736, 1942.
    • (1942) NACA Technical Report No. 736 , vol.736
    • Theodorsen, T.1    Garrick, I.E.2
  • 11
    • 0036850488 scopus 로고    scopus 로고
    • Review of state of art of smart structures and integrated systems
    • November
    • Chopra, I., "Review of State of Art of Smart Structures and Integrated Systems," AIAA Journal, vol.40, no. 11, November 2002.
    • (2002) AIAA Journal , vol.40 , Issue.11
    • Chopra, I.1
  • 12
    • 4344645668 scopus 로고    scopus 로고
    • Validation and understanding of UH-60A vibratory loads in steady level flight
    • July
    • Datta, A., and Chopra, I., "Validation and Understanding of UH-60A Vibratory Loads in Steady Level Flight," Journal of the American Helicopter Society, vol. 49, no.3, July 2004, pp.271-287.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.3 , pp. 271-287
    • Datta, A.1    Chopra, I.2
  • 13
    • 33644660569 scopus 로고    scopus 로고
    • Validation of structural and aerodynamic modeling using UH-60A airloads program data
    • January
    • Datta, A., and Chopra, I., "Validation of Structural and Aerodynamic Modeling Using UH-60A Airloads Program Data," Journal of the American Helicopter Society, vol. 51, no.1, January 2006, pp.43-58.
    • (2006) Journal of the American Helicopter Society , vol.51 , Issue.1 , pp. 43-58
    • Datta, A.1    Chopra, I.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.