摘要: Carr, L. W., and Chandrasekhara, M. S., "Design Development of a Compressible Dynamic Stall Facility," Journal Aircraft, Vol. 29, No. 3, 1992, pp. 314-318. Brock, N. J., "A Real Time Interferometry System for Unsteady Flow Measurements," ICIASF91 Record, Inst. Electrical Electronics Engineers, Publ. 91-CH-3038-8, 423-430. Goldstein, R. "Optical Systems Measurement: Shadowgraph, Schlieren Interferometric Techniques," Fluid Mechanics Measurements, Hemisphere, New York, 1983, 377-422. Lorber, P. F., Carta, F. O., "Airfoil at Constant Pitch Rate High Reynolds Number," 25, 6, 1988, 548-556.
sci-hub.se 参考文章(7)
Fort F. Felker, Martin D. Maisel, Mark D. Betzina, Full-scale tilt-rotor hover performance Journal of The American Helicopter Society. ,vol. 31, pp. 10- 18 ,(1986) , 10.4050/JAHS.31.2.10
F. X. Caradonna, C. Tung, Experimental and Analytical Studies of a Model Helicopter Rotor in Hover ,(1980)
K. Ramachandran, C. Tung, F. X. Caradonna, Rotor hover performance prediction using a free-wake, computational fluid dynamics method Journal of Aircraft. ,vol. 26, pp. 1105- 1110 ,(1989) , 10.2514/3.45887
Anton J. Landgrebe, The Wake Geometry of a Hovering Helicopter Rotor and its Influence on Rotor Performance Journal of The American Helicopter Society. ,vol. 17, pp. 3- 15 ,(1972) , 10.4050/JAHS.17.3
Alexander H. Flax, Vortex and momentum theories for hovering rotors Journal of Aircraft. ,vol. 32, pp. 1413- 1414 ,(1995) , 10.2514/3.8294
John L. Hess, Walter O. Valarezo, Calculation of Steady Flow About Propellers Using a Surface Panel Method Journal of Propulsion and Power. ,vol. 1, pp. 470- 476 ,(1985) , 10.2514/3.22830
D. Favier, A. Ettaouil, C. Maresca, Numerical and experimental investigation of isolated propeller wakesin axial flight Journal of Aircraft. ,vol. 26, pp. 837- 846 ,(1989) , 10.2514/3.45849