A Method for Studying the Transient Blade-Flapping Behavior of Lifting Rotors at Extreme Operating Conditions Page: 18 of 28
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3N
NACA TN 3366 17
REE RENCES
1. Bennett, J. A. J.: Rotary-Wing Aircraft . V.- Flapping. Aircraft
Engineering, vol. XII, no. 135, May 1940, pp. 139-141, 146.
2. Horvay, Gabriel: Rotor Blade Flapping Motion. Quarterly Appl. Math.,
vol. V, no. 2, July 1947, pp. 149-167.
3. Horvay, Gabriel, and Yuan, S. W.: Stability of Rotor Blade Flapping
Motion When the Hinges Are Tilted. Generalization of the "Rectangular
Ripple" Method of Solution. Jour. Aero. Sci., vol. 14, no. 10,
Oct. 1947, pp. 583-593.
4. Parkus, Henry: The Disturbed Flapping Motion of Helicopter Rotor
Blades. Jour. Aero. Sci., vol. 15, no. 2, Feb. 1948, pp. 103-106.
5. Yuan, S. W., and Morduchow, M.: On the Stability of the Transient
Motion of Helicopter Blades in Flapping and lagging. Reissner
Anniversary Vol.: Contributions to Applied Mechanics. J. W. Edwards
(Ann Arbor, Mich.), 1949, pp. 163-181.
6. Scarborough, James B.: Numerical Mathematical Analysis. Second ed.,
The John Hopkins Press (Baltimore), 1950, pp. 299-3035
7. Pope, Alan: Summary Report of the Forces and Moments Over an NACA
0015 Airfoil Through 180 Angle of Attack. Aero Digest, vol. 58,
no. 4, Apr. 1949, pp. 76-78, 100.
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Gessow, Alfred & Crim, Almer D. A Method for Studying the Transient Blade-Flapping Behavior of Lifting Rotors at Extreme Operating Conditions, report, January 1955; (https://digital.library.unt.edu/ark:/67531/metadc56061/m1/18/: accessed April 19, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.