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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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Lachmann, Pergamon Press, N.Y., 1961.
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Flow - A New Method of Uniparametric Calculation, ARC R & M 2587, 1952.
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laminaren Reibungsschicht mit Absaugung, Forsch. Ing.-Wes.,
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die Berechnung laminaren Grenzschichten, Bericht № 34 der Deutschen
Versuchsanstalt fur Luftfahrt, 1957.
51. T h w a i t e s B., A Theoretical Discussion of High-lift Aerofoils
with Leading-edge Porous Suction, ARC R & M 2242, London, 1946.
52. Poppleton E. D., Boundary-layer Control for High Lift by Suction at
the Leading Edge of a 40° Sweep-back Wing, ARC R & M 2897, London, 1951.
232
ГЛАВА XII
53. Groth Е. Е., Boundary Layer Suction Experiments at Supersonic Speeds,
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1, ed. by G. V., Lachmann, Pergamonn Press, N.Y., 1961.
55. С h a p m a n D. R., A Theoretical Analysis of Heat Transfer in
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62. Ringleb F. 0., Two-dimensional Flow with Standing Vortices in Ducts
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seventh ser. (July 1952).
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Bluff Body at Incidence by Means of a Spike, Royal Aircraft Establishment
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of Scientific Research, Waschington, DC, Rept, AFOSR 307, June 1961.
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Supersonic Air Speeds, the David Taylor Model Basin Aero. Rept, 925,
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67. В r i n d 1 e С. С., M a 1 i a M. J., Longitudinal Aerodynamic and
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