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Volumn 55, Issue 3, 2010, Pages 0320081-03200811

Dynamic blade shape for improved helicopter rotor performance

Author keywords

[No Author keywords available]

Indexed keywords

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

EID: 77956149022     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.55.032008     Document Type: Article
Times cited : (53)

References (24)
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    • (2005) Aeromechanics of the Active Elevon Rotor
    • Fulton, M.V.1
  • 4
    • 43749097040 scopus 로고    scopus 로고
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    • April
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    • Yeo, H.1
  • 7
    • 77956147366 scopus 로고    scopus 로고
    • AHS Aerodynamic, Acoustics, and Test and Evaluation Technical Specialists' Meeting, San Francisco, CA, January 23-25
    • Yeo, H., and Lim, J. W., "Application of a Slotted Airfoil for UH-60A Helicopter Performance:' AHS Aerodynamic, Acoustics, and Test and Evaluation Technical Specialists' Meeting, San Francisco, CA, January 23-25 2002.
    • (2002) Application of a slotted airfoil for UH-60A helicopter performance
    • Yeo, H.1    Lim, J.W.2
  • 11
    • 30744457626 scopus 로고    scopus 로고
    • AIAA 2005-1365, 43rd AIAA Aerospace Sciences Meeting, Reno, NV, January 10-13
    • Kerho M., "Adaptive Airfoil Dynamic Stall Control," AIAA 2005-1365, 43rd AIAA Aerospace Sciences Meeting, Reno, NV, January 10-13, 2005.
    • (2005) Adaptive Airfoil Dynamic Stall Control
    • Kerho, M.1
  • 12
    • 0024302234 scopus 로고
    • Higher harmonic control: Wind tunnel demonstration of fully effective vibratory hub force suppression
    • January
    • Shaw, J., Albion, N., Hanker, E. J., and Teal, R. S., "Higher Harmonic Control: Wind Tunnel Demonstration of Fully Effective Vibratory Hub Force Suppression:' Journal of the American Helicopter Society, Vol. 34, (1), January 1989, pp. 14-25.
    • (1989) Journal of the American Helicopter Society , vol.34 , Issue.1 , pp. 14-25
    • Shaw, J.1    Albion, N.2    Hanker, E.J.3    Teal, R.S.4
  • 13
    • 0025251978 scopus 로고
    • Application of higher harmonic control to rotors operating at high speed and thrust
    • Nguyen, K., and Chopra, I., "Application of Higher Harmonic Control to Rotors Operating at High Speed and Thrust," Journal of the American Helicopter Society, Vol. 35, (3), 1990, pp. 78-89.
    • (1990) Journal of the American Helicopter Society , vol.35 , Issue.3 , pp. 78-89
    • Nguyen, K.1    Chopra, I.2
  • 14
    • 0019703289 scopus 로고
    • Higher harmonic control for helicopters with two bladed and four-bladed rotors
    • Yen, J. G., "Higher Harmonic Control for Helicopters with TwoBladed and Four-Bladed Rotors:' Journal ofAircraft, Vol. 18, (12), 1981, pp. 1064-1069.
    • (1981) Journal of Aircraft , vol.18 , Issue.12 , pp. 1064-1069
    • Yen, J.G.1
  • 15
    • 0026141667 scopus 로고
    • A study of fundamental issues in higher harmonic control using aeroelastic simulation
    • April
    • Robinson, L. H., and Friedmann, P. P., "A Study of Fundamental Issues in Higher Harmonic Control Using Aeroelastic Simulation," Journal of American Helicopter Society, Vol. 36, (2), April 1991, pp. 32-43.
    • (1991) Journal of American Helicopter Society , vol.36 , Issue.2 , pp. 32-43
    • Robinson, L.H.1    Friedmann, P.P.2
  • 23
    • 38149107533 scopus 로고    scopus 로고
    • Lift enhancement with static extended trailing edge
    • November-December
    • Liu T., Montefort, J., Liou, W., and Pantula, S. R., "Lift Enhancement with Static Extended Trailing Edge," Journal of Aircraft, Vol. 44, (6), November-December 2007, pp. 1939-1947.
    • (2007) Journal of Aircraft , vol.44 , Issue.6 , pp. 1939-1947
    • Liu, T.1    Montefort, J.2    Liou, W.3    Pantula, S.R.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.