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Volumn 3, Issue , 2009, Pages 1921-1939

Reducing trailing edge flap deflection requirements in swashplateless primary control with a moveable horizontal tail

Author keywords

[No Author keywords available]

Indexed keywords

CURRENT ACTUATORS; FIXED FRAMES; FORWARD SPEED; HIGH SPEED FLIGHT; MAINTENANCE REQUIREMENT; NONDIMENSIONAL; PERFORMANCE PENALTIES; PRIMARY CONTROL; RIGID ROTATION; ROTATING NATURAL FREQUENCY; TRAILING EDGE FLAPS;

EID: 70350496634     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (22)
  • 1
    • 10944267141 scopus 로고    scopus 로고
    • Aeroelastic Modeling of Trailing-Edge-Flap Helicopter Rotors Including Actuator Dynamics
    • Nov-Dec
    • Shen, J. and Chopra, I., "Aeroelastic Modeling of Trailing-Edge-Flap Helicopter Rotors Including Actuator Dynamics," Journal of Aircraft, Vol. 41, (6), Nov-Dec 2004.
    • (2004) Journal of Aircraft , vol.41 , Issue.6
    • Shen, J.1    Chopra, I.2
  • 4
    • 70350470640 scopus 로고    scopus 로고
    • Shen, J., Comprehensive Aeroelastic Analysis of Helicopter Rotor with Trailing Edge Flap for Primary Control and Vibration Control, University of Maryland, Department of Aerospace Engineering, College Park, MD, PhD Thesis 2003.
    • Shen, J., "Comprehensive Aeroelastic Analysis of Helicopter Rotor with Trailing Edge Flap for Primary Control and Vibration Control," University of Maryland, Department of Aerospace Engineering, College Park, MD, PhD Thesis 2003.
  • 5
    • 4143136368 scopus 로고    scopus 로고
    • A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing Edge Flaps
    • Montreal, Canada, June
    • Shen, J., "A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing Edge Flaps," American Helicopter Society 58th Annual Forum Proceedings, Montreal, Canada, June 2002.
    • (2002) American Helicopter Society 58th Annual Forum Proceedings
    • Shen, J.1
  • 6
    • 4143109029 scopus 로고    scopus 로고
    • Actuation Requirements of Swashplateless Trailing-Edge Flap Helicopter Rotor in Maneuvering and Autorotation Flight
    • Baltimore, MD, Jun
    • Shen, J. and Chopra, I., "Actuation Requirements of Swashplateless Trailing-Edge Flap Helicopter Rotor in Maneuvering and Autorotation Flight," American Helicopter Society 60th Annual Forum Proceedings, Baltimore, MD, Jun 2004.
    • (2004) American Helicopter Society 60th Annual Forum Proceedings
    • Shen, J.1    Chopra, I.2
  • 7
    • 0010201010 scopus 로고    scopus 로고
    • Aeroelastic Considerations for Rotorcraft Primary Control with On-Blade Elevons
    • Washington, DC, May
    • Ormiston, R., "Aeroelastic Considerations for Rotorcraft Primary Control with On-Blade Elevons," American Helicopter Society 57th Annual Forum Proceedings, Washington, DC, May 2001.
    • (2001) American Helicopter Society 57th Annual Forum Proceedings
    • Ormiston, R.1
  • 11
    • 84884308596 scopus 로고    scopus 로고
    • Trailing Edge Flaps for Active Rotor Control Aeroelastic Characteristics of the ADASYS Rotor System
    • Phoenix, AZ, May
    • Deiterich, O. and Enenkl, B., "Trailing Edge Flaps for Active Rotor Control Aeroelastic Characteristics of the ADASYS Rotor System," American Helicopter Society 62nd Annual Forum Proceedings, Phoenix, AZ, May 2006.
    • (2006) American Helicopter Society 62nd Annual Forum Proceedings
    • Deiterich, O.1    Enenkl, B.2
  • 12
    • 4143083696 scopus 로고    scopus 로고
    • Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade FLapping
    • Baltimore, MD, Jun
    • Gandhi, F., "Helicopter Horizontal Tail Incidence Control to Reduce Rotor Cyclic Pitch and Blade FLapping," American Helicopter Society 60th Annual Forum Proceedings, Baltimore, MD, Jun 2004.
    • (2004) American Helicopter Society 60th Annual Forum Proceedings
    • Gandhi, F.1
  • 13
    • 0003866245 scopus 로고    scopus 로고
    • Nonstationary Flow About a Wing-Aileron-Tab Combination Including Aerodynamic Balance,
    • No. 736 1942
    • Theodorsen, T. and Garrick, I., "Nonstationary Flow About a Wing-Aileron-Tab Combination Including Aerodynamic Balance," NACA Technical Report No. 736 1942.
    • NACA Technical Report
    • Theodorsen, T.1    Garrick, I.2
  • 17
    • 84884407683 scopus 로고    scopus 로고
    • An Investigation Into the Aerodynamics of Trailing Edge Flap and Flap-Tab Airfoils Using CFD and Analytical Methods
    • Virginia Beach, VA, May
    • Jose, A., Sitaraman, J., and Baeder, J., ""An Investigation Into the Aerodynamics of Trailing Edge Flap and Flap-Tab Airfoils Using CFD and Analytical Methods," American Helicopter Society 63rd Annual Forum Proceedings, Virginia Beach, VA, May 2007.
    • (2007) American Helicopter Society 63rd Annual Forum Proceedings
    • Jose, A.1    Sitaraman, J.2    Baeder, J.3
  • 18
    • 14044252803 scopus 로고    scopus 로고
    • Experimental/Numerical Evaluation of Integral Trailing Edge Flaps for Helicopter Rotor Applications
    • Jan
    • 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, (1), Jan 2005.
    • (2005) Journal of the American Helicopter Society , vol.50 , Issue.1
    • Hassan, A.1    Straub, F.2    Noonan, K.3
  • 19
  • 21
    • 1842474695 scopus 로고    scopus 로고
    • UH-60 Black Hawk Engineering Simulation Program,
    • 166309 Dec 1981
    • Howlett, J., "UH-60 Black Hawk Engineering Simulation Program," NASA Contractor Report 166309 Dec 1981.
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    • Howlett, J.1
  • 22
    • 4344606344 scopus 로고    scopus 로고
    • Performance Analysis of a Utility Helicopter with Standard and Advanced Rotors
    • July
    • Yeo, H., Bousman, W., and Johnson, W., "Performance Analysis of a Utility Helicopter with Standard and Advanced Rotors," Journal of the American Helicopter Society, Vol. 49, (3), July 2004.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.3
    • Yeo, H.1    Bousman, W.2    Johnson, W.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.