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Volumn 1, Issue , 2008, Pages 148-171

Application of hybrid methodology to rotors in steady and maneuvering flight

Author keywords

[No Author keywords available]

Indexed keywords

CONVERGENCE CHARACTERISTICS; FLIGHT CONDITIONS; FORWARD FLIGHT; HYBRID METHODOLOGY; LOOSE COUPLINGS; MANEUVERING FLIGHT; MAXIMUM LOADS; NORMAL FORCES; PITCHING MOMENTS; REASONABLE AGREEMENT; TEST DATA;

EID: 50249187623     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (40)

References (17)
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    • Potsdam, M.1    Yeo, H.2    Johnson, W.3
  • 2
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    • CFD Based Unsteady Aerodynamic Modeling for Rotor Aeroelastic Analysis
    • Ph. D. Dissertation, University of Maryland
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    • (2003)
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  • 4
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    • Phanse, Sujeet, Sankar, Lakshmi N., Charles, B.D.,Efficient Coupled Fluid Structure Interaction Approach for Analysis of Rotors in Forward Flight, American Helicopter Vertical Lift Aircraft Design Conference, San Francisco, California, January 18-29, 2006
    • Phanse, Sujeet, Sankar, Lakshmi N., Charles, B.D.,"Efficient Coupled Fluid Structure Interaction Approach for Analysis of Rotors in Forward Flight", American Helicopter Vertical Lift Aircraft Design Conference, San Francisco, California, January 18-29, 2006
  • 5
    • 34250799119 scopus 로고    scopus 로고
    • Duque, E., Sankar, L. N., Menon, S., Bauchau, O., Ruffin, S., Smith, M., Ahuja, K., Brentner, K., Long, L., Morris, P., and Gandhi, F., Revolutionary Physics-Based Design Tools for Quiet Helicopters, 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA, Reno, NV, January 2006, AIAA 2001-1068.
    • Duque, E., Sankar, L. N., Menon, S., Bauchau, O., Ruffin, S., Smith, M., Ahuja, K., Brentner, K., Long, L., Morris, P., and Gandhi, F., "Revolutionary Physics-Based Design Tools for Quiet Helicopters," 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA, Reno, NV, January 2006, AIAA 2001-1068.
  • 6
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    • Bhagwat, M., J. ,Ormiston , R. A., Saberi, H. A. and Hong, X., Application of CFD/CSD Coupling for Analysis of Rotorcraft Airloads and Blade Loads in Maneuvering Flight, AHS 63rd Annual Forum, Virginia Beach, VA, 2007
    • Bhagwat, M., J. ,Ormiston , R. A., Saberi, H. A. and Hong, X., "Application of CFD/CSD Coupling for Analysis of Rotorcraft Airloads and Blade Loads in Maneuvering Flight", AHS 63rd Annual Forum, Virginia Beach, VA, 2007
  • 8
    • 50249171084 scopus 로고    scopus 로고
    • Bousman, William G. and Kufeld, Robert M., UH-60A Airloads Catalog, Aeroflightdynamics Directorate (AMRDEC), U.S. Army Research, Development, and Engineering Command, Ames Research Center, Moffet Field, California, August 2005, NASA-TM-2005-212827, AFDD/TR-05-003
    • Bousman, William G. and Kufeld, Robert M., "UH-60A Airloads Catalog," Aeroflightdynamics Directorate (AMRDEC), U.S. Army Research, Development, and Engineering Command, Ames Research Center, Moffet Field, California, August 2005, NASA-TM-2005-212827, AFDD/TR-05-003
  • 9
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    • A Hybrid Flow Analysis for Rotors in Forward Flight
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    • (2001)
    • Yang, Z.1    Sankar, L.2
  • 10
    • 0018281328 scopus 로고
    • What are the Lift and Propulsive Force Limits at High Speed for the Conventional Rotor?
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    • McHugh, F.J.1
  • 11
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    • (2008) AHS Specialist's Conference on Aeromechanics
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  • 12
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    • Nygaard, Tor A., Saberi, Hossein, Ormiston, Robert A., Strawn, Roger C., Potsdam, Mark, and Johnson, Wayne, Fluid Structure Interface for Rotorcraft Aeromechanic Computations, Unpublished Report, ELORET Corp., Advanced Rotorcraft Technology, AMRDEC, NASA-Ames Research Center, May 3, 2005
    • Nygaard, Tor A., Saberi, Hossein, Ormiston, Robert A., Strawn, Roger C., Potsdam, Mark, and Johnson, Wayne, "Fluid Structure Interface for Rotorcraft Aeromechanic Computations," Unpublished Report, ELORET Corp., Advanced Rotorcraft Technology, AMRDEC, NASA-Ames Research Center, May 3, 2005
  • 13
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    • April
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    • Kufeld, R.M.1    Bousman, W.G.2
  • 15
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.