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Volumn II, Issue , 2006, Pages 935-953

Assessment of active controls for rotor performance enhancement

Author keywords

[No Author keywords available]

Indexed keywords

CAMRAD II; GURNEY FLAP; LOADING CAPABILITY; OSCILLATORY JET;

EID: 33748462660     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (29)
  • 6
    • 84883493556 scopus 로고    scopus 로고
    • Hybrid pulsed suction/pulsed blowing jets for improved airfoil stall/post stall aerodynamics
    • Grapevine, TX, June
    • Hassan, A. A., "Hybrid Pulsed Suction/Pulsed Blowing Jets for Improved Airfoil Stall/Post Stall Aerodynamics," Proceedings of the American Helicopter Society 61st Annual Forum, Grapevine, TX, June 2005.
    • (2005) Proceedings of the American Helicopter Society 61st Annual Forum
    • Hassan, A.A.1
  • 7
    • 84884295477 scopus 로고
    • The potential of gurney flaps for improving the aerodynamic performance of helicopter rotors
    • AIAA Paper No. 1993-4883
    • "The Potential of Gurney Flaps for Improving the Aerodynamic Performance of Helicopter Rotors," Proceedings of the AIAA International Powered Lift Conference, AIAA Paper No. 1993-4883, 1993.
    • (1993) Proceedings of the AIAA International Powered Lift Conference
  • 13
    • 0030828202 scopus 로고    scopus 로고
    • Wind tunnel testing of a smart rotor with induced strain actuation of blade twist
    • Chen, P. C., and Chopra, I., "Wind Tunnel Testing of a Smart Rotor with Induced Strain Actuation of Blade Twist," AIAA Journal, Vol. 35(1), pp. 6-16, 1997.
    • (1997) AIAA Journal , vol.35 , Issue.1 , pp. 6-16
    • Chen, P.C.1    Chopra, I.2
  • 19
    • 0032184345 scopus 로고    scopus 로고
    • Rotors with trailing edge flaps: Analysis and comparison with experimental data
    • October
    • Milgram, J., Chopra, I., and Straub, F., "Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data," Journal of the American Helicopter Society, Vol. 43, No. 4, October 1998.
    • (1998) Journal of the American Helicopter Society , vol.43 , Issue.4
    • Milgram, J.1    Chopra, I.2    Straub, F.3
  • 21
    • 14044252803 scopus 로고    scopus 로고
    • Experimental/numerical evaluation of integral trailing edge flaps for helicopter rotor application
    • January
    • Hassan, A. A., Straub, F., and Noonan, K. W., "Experimental/ Numerical Evaluation of Integral Trailing Edge Flaps for Helicopter Rotor Application," Journal of the American Helicopter Society, Vol. 50, No. 1, January 2005.
    • (2005) Journal of the American Helicopter Society , vol.50 , Issue.1
    • Hassan, A.A.1    Straub, F.2    Noonan, K.W.3
  • 24
    • 4344606344 scopus 로고    scopus 로고
    • Performance analysis of a utility helicopter with standard and advanced rotors
    • July
    • Yeo, H., Bousman, W. G., and Johnson, W., "Performance Analysis of a Utility Helicopter with Standard and Advanced Rotors," Journal of the American Helicopter Society, Vol. 49, No. 3, July 2004.
    • (2004) Journal of the American Helicopter Society , vol.49 , Issue.3
    • Yeo, H.1    Bousman, W.G.2    Johnson, W.3
  • 26
    • 33748472328 scopus 로고
    • Application of a Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics (CAMRAD) to the McDonnell douglas AH-64A helicopter
    • November
    • Callahan, C. B., "Application of a Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics (CAMRAD) to the McDonnell Douglas AH-64A Helicopter," NASA CR 177455, November 1988.
    • (1988) NASA CR 177455
    • Callahan, C.B.1
  • 28
    • 84888776017 scopus 로고
    • Newton solution of coupled viscous/inviscid multielement airfoil flows
    • June
    • Drela, M., "Newton Solution of Coupled Viscous/Inviscid Multielement Airfoil Flows," AIAA Paper No. 90-1470, June 1990.
    • (1990) AIAA Paper No. 90-1470 , vol.90 , Issue.1470
    • Drela, M.1
  • 29
    • 29544444033 scopus 로고    scopus 로고
    • Optimum two-per-revolution inputs for improved rotor performance
    • November-December
    • Cheng, R. P., and Celi, R., "Optimum Two-Per-Revolution Inputs for Improved Rotor Performance," Journal of Aircraft, Vol. 42, No. 6, November-December 2005.
    • (2005) Journal of Aircraft , vol.42 , Issue.6
    • Cheng, R.P.1    Celi, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.