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Volumn , Issue , 2004, Pages 1-15

Application of a momentum source model to the RAH-66 comanche FANTAIL

Author keywords

[No Author keywords available]

Indexed keywords

FLOW FIELDS; MACH NUMBER; ROTOR BLADES; TAIL ROTORS;

EID: 2942519506     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (23)

References (11)
  • 2
    • 85087187888 scopus 로고    scopus 로고
    • Unsteady RAH-66 comanche flowfield simulations including fan-in-fin
    • June
    • Alpman, E., Long, L. N., and Kothmann, B. D., "Unsteady RAH-66 Comanche Flowfield Simulations including Fan-in-Fin," AIAA Paper 2003-4234 , June 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.4234
    • Alpman, E.1    Long, L.N.2    Kothmann, B.D.3
  • 3
    • 0029461734 scopus 로고
    • Navier-stokes simulation of a rotor using a distributed pressure disk model
    • Fort Worth, TX, May
    • Chaffin, M. S., and Berry, J. D., "Navier-Stokes Simulation of a Rotor using a Distributed Pressure Disk Model," American Helicopter Society 51st Annual Forum, Fort Worth, TX , May 1995.
    • (1995) American Helicopter Society 51st Annual Forum
    • Chaffin, M.S.1    Berry, J.D.2
  • 4
    • 2942541088 scopus 로고    scopus 로고
    • Discrete blade CFD analysis of ducted tail fan flow
    • Jan.
    • Ruzicka, G. C. and Strawn, R. C., " Discrete Blade CFD Analysis of Ducted Tail Fan Flow," AIAA Paper 2004-48 , Jan. 2004.
    • (2004) AIAA Paper , vol.2004 , Issue.48
    • Ruzicka, G.C.1    Strawn, R.C.2
  • 5
    • 2942608945 scopus 로고
    • New aerodynamic design of the fenestron for improved performance
    • Garmisch-Partenkirchen, FRG, Sept.
    • Vuillet, A., and Morelli, F., "New Aerodynamic Design of the Fenestron for Improved Performance," 12th European Rotorcraft Forum, Garmisch-Partenkirchen, FRG, Sept. 1986.
    • (1986) 12th European Rotorcraft Forum
    • Vuillet, A.1    Morelli, F.2
  • 6
    • 0014856645 scopus 로고
    • Increasing tail rotor thrust and comments on other yaw control devices
    • Oct.
    • Robinson, F., "Increasing Tail Rotor Thrust and Comments on Other Yaw Control Devices ," Journal of the American Helicopter Society, Oct. 1970, pp. 46-52.
    • (1970) Journal of the American Helicopter Society , pp. 46-52
    • Robinson, F.1
  • 7
    • 2942542584 scopus 로고
    • BVWT 0345: Wind tunnel test on the 0.75 scale L.H.X. Fan-in-fin powered model
    • March
    • "BVWT 0345: Wind Tunnel Test on the 0.75 Scale L.H.X. Fan-in-Fin Powered Model," Boeing Report 8-7891-1-882, March 1990.
    • (1990) Boeing Report 8-7891-1-882
  • 8
    • 2942572735 scopus 로고    scopus 로고
    • RAH-66 demonstration/ validation fantail rotor whirl test report
    • Nov.
    • "RAH-66 Demonstration/ Validation Fantail Rotor Whirl Test Report," Boeing Sikorsky Document 2000-224-001, Nov. 1996.
    • (1996) Boeing Sikorsky Document 2000-224-001
  • 9
    • 85086489860 scopus 로고    scopus 로고
    • Automatic off-body grid generation for domains of arbitrary size
    • June
    • Meakin, R. L., "Automatic Off-Body Grid Generation for Domains of Arbitrary Size," AIAA Paper 2001-2536, June 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.2536
    • Meakin, R.L.1
  • 10
    • 0034730338 scopus 로고    scopus 로고
    • Adaptive spatial partitioning and refinement for overset structured grids
    • Meakin, R. L., "Adaptive Spatial Partitioning and Refinement for Overset Structured Grids," Comput. Methods Appl. Mech. Engrg., Vol. 189, No. 1077-1117, 2000.
    • (2000) Comput. Methods Appl. Mech. Engrg. , vol.189 , Issue.1077-1117
    • Meakin, R.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.