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Volumn 1, Issue , 2009, Pages 677-688

Dynamic blade shape for improved helicopter rotor performance

Author keywords

[No Author keywords available]

Indexed keywords

BLADE SHAPES; FORWARD SPEED; LOAD CAPABILITY; LOW LEVEL; MAXIMUM SPEED; MORPHING; PHYSICAL MECHANISM; ROTOR PERFORMANCE; VARIABLE ROTOR SPEED;

EID: 70449111581     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (14)
  • 1
    • 0008899146 scopus 로고    scopus 로고
    • Design of the Active Elevon Rotor for Low Vibration
    • Atlanta, GA, November 13-15
    • Fulton, M. V., "Design of the Active Elevon Rotor for Low Vibration," AHS Aeromechanics Specialists' Meeting, Atlanta, GA, November 13-15,2000.
    • (2000) AHS Aeromechanics Specialists' Meeting
    • Fulton, M.V.1
  • 3
    • 43749097040 scopus 로고    scopus 로고
    • Assessment of Active Controls for Rotor Performance Enhancement
    • April
    • Yeo, H., "Assessment of Active Controls for Rotor Performance Enhancement," Journal of American Helicopter Society, Vol. 53, No. 2, April 2008.
    • (2008) Journal of American Helicopter Society , vol.53 , Issue.2
    • Yeo, H.1
  • 5
    • 0032683384 scopus 로고    scopus 로고
    • Noonan, K. W.; Yeager, W. T., Jr.; Singleton, Jeffrey D.; Wilbur, Matthew L.; and Mirick, Paul H., Evaluation of a Model Helicopter Main Rotor Blade with Slotted Airfoils at the Tip, AHS 55th Annual Forum, Montreal, Quebec, Canada, May 25-27, 1999
    • Noonan, K. W.; Yeager, W. T., Jr.; Singleton, Jeffrey D.; Wilbur, Matthew L.; and Mirick, Paul H., "Evaluation of a Model Helicopter Main Rotor Blade with Slotted Airfoils at the Tip," AHS 55th Annual Forum, Montreal, Quebec, Canada, May 25-27, 1999
  • 6
    • 70449093146 scopus 로고
    • Effect of an Extendable Slat on the Stall Behavior of a VR-12 Airfoil
    • Sept
    • Hugues, P.P.D.H.; McAlister, K. W.; and Yung, C. "Effect of an Extendable Slat on the Stall Behavior of a VR-12 Airfoil," NASA Technical Paper 3407, Sept. 1993
    • (1993) NASA Technical Paper , vol.3407
    • Hugues, P.P.D.H.1    McAlister, K.W.2    Yung, C.3
  • 7
    • 0032661269 scopus 로고    scopus 로고
    • Design and Evaluation of Multi-Element Airfoils for Rotorcraft
    • Montreal, Quebec, Canada, May 25-27
    • Narramore, J.C.; McCroskey, W.J.; and Noonan, K.W., "Design and Evaluation of Multi-Element Airfoils for Rotorcraft," AHS 55th Annual Forum, Montreal, Quebec, Canada, May 25-27, 1999
    • (1999) AHS 55th Annual Forum
    • Narramore, J.C.1    McCroskey, W.J.2    Noonan, K.W.3
  • 8
    • 34250842688 scopus 로고    scopus 로고
    • Control of Separation on the Flap of a Three-Element High-Lift Configuration
    • Gunther, B; Thiele, F.; Petz, R.; and Nitshe, W., "Control of Separation on the Flap of a Three-Element High-Lift Configuration," AIAA 2007-265, 2007
    • (2007) AIAA , vol.2007 -265
    • Gunther, B.1    Thiele, F.2    Petz, R.3    Nitshe, W.4
  • 9
    • 70449106537 scopus 로고    scopus 로고
    • Miniature Trailing Edge Effectors for Rotorcraft Application
    • Lesieutre, G.A., "Miniature Trailing Edge Effectors for Rotorcraft Application," Presentation at PSU, 2005
    • (2005) Presentation at PSU
    • Lesieutre, G.A.1
  • 11
    • 28844456935 scopus 로고    scopus 로고
    • Dynamic Stall Measurements and Computations for a VR-12 Airfoil with a Variable Droop Leading Edge
    • Phoenix, Arizona, May 6-8
    • Martin, P.B.; McAlister, K.W.; Chandersekhara, M.S.; and Geisler, W., "Dynamic Stall Measurements and Computations for a VR-12 Airfoil with a Variable Droop Leading Edge," AHS 59th Annual Forum, Phoenix, Arizona, May 6-8, 2003
    • (2003) AHS 59th Annual Forum
    • Martin, P.B.1    McAlister, K.W.2    Chandersekhara, M.S.3    Geisler, W.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.