| Citation: | YANG Kelong, HAN Dong. Hover performance of helicopter main and tail rotors with swirl velocities[J]. Journal of Aerospace Power, 2021, 36(1): 119-129. doi: 10.13224/j.cnki.jasp.2021.01.014 |
| [1] |
LIM J W,MCALISTER K W,JOHNSON W R.Hover performance correlation for full-scale and model-scale coaxial rotors[J].Journal of the American Helicopter Society,2009,54(2):1-14.
|
| [2] |
JAIN R K,POTSDAM M A.Hover predictions on the Sikorsky S-76 rotor using helios[C]∥52nd Aerospace Sciences Meeting.Virginia Beach,US:AIAA,2011:66-78.
|
| [3] |
JIMENZ G A,BARAKOS G N.Accurate predictions of rotor hover performance at low and high disc loadings[J].Journal of Aircraft,2018,55(3):89-110.
|
| [4] |
MCCUTCHEN C W.A theorem on swirl loss in propeller wakes[J].Journal of Aircraft,1985,22(6):344-346.
|
| [5] |
FRANCOIS B,LABAN M,COSTES M D G.In-plane forces prediction and analysis in high-speed conditions on a contra-rotating open rotor[J].Journal of Turbomachinery,2014,136(5):1-16.
|
| [6] |
JOHNSON W R.Helicopter theory[M].New York:Dover Publications,1994:40-45.
|
| [7] |
LUCAS F.Study of counter-rotating coaxial rotors in hover:a performance model based on blade element theory including swirl velocity[D].Daytona Beach,US:Embry-Riddle Aeronautical University,2007.
|
| [8] |
STAHLHUT C,LEISHMAN J G.Aerodynamic design optimization of proprotors for convertible-rotor concepts[C]∥68th American Helicopter Society Annual Forum.Dallas,US:Vertical Flight Society,2012:593-616.
|
| [9] |
MODARRES R,PETERS D A.Optimum actuator-disk performance in hover and axial flight by a compact momentum theory with swirl[J].Journal of the American Helicopter Society,2015,60(4):1-10.
|
| [10] |
PETERS D A,HAQUANG N.Dynamic inflow for practical applications[J].Journal of the American Helicopter Society,1988,33(4):64-68.
|
| [11] |
LEISHMAN J G.Principles of helicopter aerodynamics[M].3th ed.New York:Cambridge University Press,2006:62-64.
|
| [12] |
HAN Dong,PASTRIKAKIS V,BARAKOS G N.Helicopter flight performance improvement by dynamic blade twist[J].Aerospace Science and Technology,2016,58(2):445-452.
|
| [13] |
HAN Dong,DONG Chen,BARAKOS G N.Performance improvement of variable speed rotors by gurney flaps[J].Aerospace Science and Technology,2018,81(5):118-127.
|
| [14] |
DONG Chen,HAN Dong,YU Lei.Performance analysis of variable speed tail rotors with gurney flaps[J].Chinese Journal of Aeronautics,2018,31(7):4-10.
|
| [15] |
YEO H,BOUSMAN W G,JOHNSON W R.Performance analysis of a utility helicopter with standard and advanced rotors[J].Journal of the American Helicopter Society,2004,49(6):250-270.
|
| [16] |
SHINODA P M,YEO H,NORMAN T R.Rotor performance of a UH-60A rotor system in the NASA MES 80-by 120-foot wind tunnel[J].Journal of the American Helicopter Society,2004,49(6):401-413.
|
| [17] |
HILBERT K B.A mathematical model of the UH-60 helicopter[R].NASA-TM-85890,1984.
|
| [18] |
DAVIS S J.Pedesign study for a modern 4-bladed rotor for the RSRA[R].NASA-CR-166155,1981.
|
| [19] |
JOHNSON W R.Rotorcraft aeromechanics[M].New York:Cambridge University Press,2013:48-52.
|
| [20] |
BUCKANIN R M,HERBST M K,LOCKWOOD R A,et al.Airworthiness and flight characteristics test of a sixth year production UH-60A[R].Washington DC:USA AEFA Project No.83-24,1985.
|
| [21] |
NAGATA J I,PIOTROWSKI J L,YOUNG C J,et al.Baseline performance verification of the 12th year production UH-60A black hawk helicopter[R].Washington DC:USA AEFA Project No.87-32,1989.
|
| [22] |
BOUSMAN W G.Power measurement errors on a utility aircraft[C]∥Proceedings of 3rd American Helicopter Society Aerodynamics,Acoustics,and Test and Evaluation Technical Specialists Meeting.San Francisco,US:Vertical Flight Society,2002:35-48.
|