1 |
Lee, D. J. and Na, S. U., 'High Resolution Free Vortex Blob Method for Highly Distorted Vortex Wake Generated from a Slowly Starting Rotor Blade in Hover', 21st European Rotorcraft Forum, St. Petersburg, Russia, Aug, 30-Sept. 1, 1995
|
2 |
Lee, D. J. and Na, S. U., 'Numerical Simulation of Wake Structure Generated by Rotating Blades Using a Time-Marching Free-Blob Method', European J. Fluid Mech. -B/Fluids, 17 (4), pp. 1-13
|
3 |
Peters, D. A., Boyd, D. D. and He, C. J., 'Finite-State Induced-Flow Model for Rotors in Hover and Forward Flight', 43rd Annual Forum of American Helicopter Soc., St. Louis, MO, May 18-20, 1987
|
4 |
Peters, D. A and He, C. J., 'Finite-State Induced-Flow Models Part II: Three-Dimensional Rotor Disk', J. of Aircraft, 32 (2), March-April, pp. 323-333. 1995
DOI
ScienceOn
|
5 |
남화진, 박영민, 권오준, '바정렬 적응 격자계를 이용한 비정상 로터-동체 공력 상호작용 모사', 한국항공우주학회지, 제 33권 제 2호, 2005, pp. 11-21
|
6 |
Leishman, J. G., Principles of Helicopter Aerodynamics, 1st Edition, Cambridge University Press 2000
|
7 |
Chung, K., Hwang, C., Lee, D.J. and Yim J., 'Numerical Investigation on a Rotor Tip-Vortex Instability in Very Low Advance Ratio Flight,' KSAS International Journal, Vol. 6, (2), pp. 84-96, 2005
|
8 |
Elliott, J.W., Althoff, S.L. and Sailey, R.H., 'Inflow Measurement Made with a Laser Velocimeter on a Helicopter Model in Forward Flight- =0.15', NASA TM 100541, 1988
|
9 |
Elliott, J. W., Althoff, S. L. and Sailey, R. H., 'Inflow Measurement Made with a Laser Velocimeter on a Helicopter Model in Forward Flight- =0.23', NASA TM 100542, 1988
|
10 |
Kocurek, J. D. and TangIer, J. L., 'A Prescribed Wake Lifting Surface Hover Performance Analysis', J. American Helicopter Soc., 22, (1), Jan., 1977, pp. 24-35
DOI
|
11 |
Felker, F. F., Quackenbush, T. R., Bliss, D. B., and Light, J. L., 'Comparisons of Predicted and Measured Rotor Performance Using a New Free Wake Method,' Proc. 44th Forum of the American Helicopter Society, Washington, D.C., June, 1988
|
12 |
Clark, D. R. and Leiper, A. C., 'The Free Wake Analysis a Method for The Prediction of Helicoper Roter Hovering Performance,' J. American Helicopter Soc., 15, (1), Jan., 1970, pp. 3-11
DOI
|
13 |
Bramwell, A R. S., Helicopter Dynamics, Edward Arnold, London, 1976
|
14 |
Bagai, A., Leishman, J. G., 'Rotor Free-Wake Modeling Using a Pseudo-Implicit Technique Including Comparisons with Experimental Data', J. American Helicopter Soc., 40, (3), July, 1995, pp. 29-41
DOI
|
15 |
Elliott, J. W., Althoff, S. L. and Sailey, R. H., 'Inflow Measurement Made with a Laser Velocimeter on a Helicopter Model in Forward Flight- =0.30', NASA TM 100543, 1988
|
16 |
Baron, A., Boffadossi M., 'Unsteady Free Wake Analysis of Closely Interacting Helicopter Rotors,' Proc. 19th European. Rotorcraft Forum, Cernobbio (Como), Italy, Sept. 14-16, 1993
|
17 |
Glauert, H., 'A General Theory of the Autogiro', ARC R&M 1111, 1926
|
18 |
Rosen, A. and Grabe, A., 'Free Wake Model of Hovering Rotors Having Straight or Curved Blades,' J. American Helicopter Soc., 33, (3), July, 1988, pp. 11-19
DOI
|
19 |
Scully, M. P., 'Computation of Helicopter Rotor Wake Geometry and Its Influence on Rotor Harmonic Airloads,' MIT ASRL TR 178-1, March, 1975
|
20 |
Drees, J. M., 'A Theory of Airflow Through Rotors and Its Application to Some Helicopter Problems', J. Helicoopter Assoc. Great Britain, 3(2), July-Sept
|
21 |
Stepniewski, W. Z. and Keys, C. N., Rotary-Wing Aerodynamics, Dover, New York, Part 1, Chapter 5
|
22 |
Landgrebe, A. J., 'The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance,' J. American Helicopter Soc., 17, (4), Oct., 1972, pp. 3-15
DOI
|
23 |
Mangler, K. W. and Squire, H. B., 'The Induced Velocity Field of a Rotor', ARC R&M 2642, 1950
|