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Отрывные течения. Том 3 - Чжен П.

Чжен П. Отрывные течения. Том 3 — М.: Мир, 1973. — 334 c.
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Rectangular Wings of Small Aspect Ratio, Z. angew¦ Math. Mech., 19, № 1,
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Ing.-Archiv., 30, № 6, 431-452 (1961).
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1955).
6. В г о w n С. E., Michael W. H., On Slender Delta Wings with Lea-ding-
edge Separation, NACA TN 3430, April 1955.
230
ГЛАВА XII
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15. Ktichemann D., A Simple Method of Calculating the Span and Chord-wise
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17. С о о к e J. С., В r e b n e r G. G., The Nature of Separation and
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18. S t r a t f о r d B. S., An Experimental Flow with Zero Skin Friction
Throughout its Region of Pressure Rise, J. Fluid Mech., 5, 17 (1959).
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narprofilen fiir Segelflugzsuge und Hubschrauber, Z. Wiss., 5, № 8, 228-
243 (Aug. 1957); также British MOS translation TIL/T, A 906.
20. P e a г с e у H. H., Shock-induced Separation and its Prevention by
Design and Boundary Layer Control, Boundary Layer and Flow Control, Vol.
2, ed. by G. V. Lachmann, Pergamon Press, N. Y., 1961.
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"УПРАВЛЕНИЕ ОТРЫВОМ ПОТОКА
231
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NACA TN 3169, July 1954.
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34. I g 1 i s с h R., Exakte Berechnung der laminaren Reibungschicht
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Akad. Luft. Forsch., 8, № 1, (1944); также NACA TM 1205, 1949.
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