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Отрывные течения. Том 1 - Чжен П.

Чжен П. Отрывные течения. Том 1 — М.: Мир, 1972. — 300 c.
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88. Eichelbrenner E., Decollement et recollement turbulent en trois
dimensions, Becherche aeronaut., № 84, p. 19 (Sept.- Oct 1961).
89. J о h n s t о n J. P., Three-dimensional Turbulent Boundary Layer,
Sc. D. thesis, MIT, May 1957.
90. Taylor E. S., The Skewed Boundary Layer, J. Basic Engng, Trans. ASME,
Ser. D, 81, pp. 297-304 (1959).
91. J о h n s t о n J. P., On the Three-dimensional Turbulent Boundary
Layer Generated by Secondary Flow, J. Basic Engng, Trans. ASME, Ser. D,
82, pp. 233-248 (1960).
92. Squire H. B., W i n t e г K. G., The Secondary Flow in a Cascadeof
Airfoils in a Non-uniform Stream, J. Aeronaut. Sci., 18, pp. 271-277
(1951).
93. R u b e г t K. F-, Persh J., A Procedure for Calculation of the
Development of Turbulent Boundary Layers under the Influence of Adverse
Pressure Gradients, NACA TN 2478 (Sept. 1951).
94. Mager A., Generalization of Boundary Layer Momentum Integral
Equations of Three-dimensional Flows Including Those of Rotating Systemg
NACA Rept 1067, 1952.
208
ГЛАВА IV
95. М a g е г A., Mahoney I. I., Budinger R. Е., Discussion of Boundary
Layer Characteristics Near the Wall of an Axial-flow Compressor, NACA
Rept 1085, 1952.
96. Himmelskamp H., Profiluntersuchungen an einem umlaufenden Propeller,
Thesis, Gottingen, 1945.
97. T а у 1 о г E. S., The Skewed Boundary Layer, ASME Paper 58-A-113,
Dec. 1958.
98. L i e b 1 e i n E., Loss and Stall Analysis of Compressor Cascade, J.
Basic Engng, Trans. ASME, Ser. D, 81, № 3 (Sept. 1959).
99. L u b i с к R. J., W a 1 1 n e r L. F., Stall Prediction in
Gas Turbine
Engines, J. Basic Engng, Trans. ASME, Ser. D, 81, № 3 (Sept. 1959).
100. Henry J. R., Wilbur S. W., Preliminary Investigation of the Flow in
an Annular-diffuser-tailpipe Combination with an Abrupt Area Expansion
and Suction, Injection, and Vortex Generator Flow Controls, NACA RM L-
53K30, 1954.
101. Herzog J., Investigation of Annular Diffusers, MaschBau Warmew., № 7
(1956).
102. U r a m E. М., The Growth of an Axisymmetric Turbulent
Boundary
Layer in an Adverse Pressure Gradient, Proc. Second US National Con-
gress of Applied Mechanics, Ann Arbor, Mich., 1954.
103. Wilbur S. W., Higginbotham J. Т., Investigation of Two Short Annular
Diffuser Configurations Utilizing Suction and Injection as a Means of
Boundary Layer Control, NACA RM L54K18, Jan. 1955.
104. Wood С. C., Higginbotham J. Т., Effects of Diffuser and Centerbody
Length on Performance of Annular Diffusers with Constant-diameter Outer
Walls and with Vortexgenerator Flow Controls, NACA RM L54G21, Sept. 1954.
105. Wood С. C., Higginbotham J. Т., The Influence of Vortex Generators
on the Performance of a Short 1.9 : 1 Straight-wall Annular Diffuser with
a Whirling Inlet Flow, NACA RM L52L01a, Feb. 1953.
106. M i 1 1 i a t J. P., Turbulent Air Flow in a Pipe with Diffusing
Section, Houille blanche, 11 (1956).
107. Wieghardt K., Betrachtungen zum Zahigkeitswiderstand von Schiffen,
Jahrbuch der Schiffbautechnischen Gesellschaft, 52 (1959).
108. Шлихтинг Г., Теория пограничного слоя, изд-во "Наука", 1964.
109. Rotta J. С., Turbulent Boundary Layers in Incompressible Flow,
Progress in Aeronautical Sciences, Vol. 2, Boundary Layer Problems, ed.
Ferry A., Kuchemann D., Sterne L. T. G., Pergamon Press, 1962.
ДОПОЛНИТЕЛЬНАЯ ЛИТЕРАТУРА
Crockrell D. J., Markland E., The Effects of Inlet Conditions on
Incompressible Fluid Flow through Conical Diffusors, J. Boy. Aeronaut.
Soc., pp. 51-52 (Jan. 1962).
Eichelbrenner E. A., Peube J. L., Theoretical and Experimental
Investigations in Three-dimensional (Laminar and Turbulent) Boundary
Layers, in Particular on Problems of Transition, Separation and Rcattach-
ment, Faculte des Sciences de Poitiers, Laboratoire de Mecanique des
Fluides (Sept. 1966).
Moses H. L., Chappell J. R., Goldberger Т., Boundary-Layer Separation in
Internal Flow, Gas Turbine Laboratory, MIT, Rept JM° 81 (Sept. 1965).
Murphy J. S., The Separation of Axially Symmetric Turbulent Boundary
Layers, Part 1: Preliminary Experimental Results on Several Bodies in
Incompressible Flow, Douglas Aircraft Div., Rept Ns ES17513, 19 March
1954.
ОТРЫВ ТУРБУЛЕНТНОГО ПОТОКА ЖИДКОСТИ
209
Robertson J. М., Prediction of Turbulent Boundary-layer Separation, J.
Aeronaut. Sci., 24, № 8, pp. 631-632 (Aug. 1957).
Рошке, Мэсси p, Отрыв потока в профилированном сопле, Ракетная техника, №
10 (1962).
Spangenberg W. G., Rowland W. R., Mease N. E., Measurements in a
Turbulent Boundary Layer Maintained in a Nearly Separating Condition,
reprinted from Fluid Mechanics of Internal Flow, Elsevier Publishing Co.,
Amsterdam, 1967.
Stratford D. S., The Prediction of Separation of the Turbulent Boundary
Layer, J. Fluid Mech., p. 17 (Jan. 1959).
S u n 1 e у H. L. G., Ferriman V. N., Jet Separation in Conical
Nozzles,
J. Roy. Aeronaut. Soc., p. 808 (Dec. 1964).
Yang, Tah-Teh, Splitter Effect in Conical Diffusers. Part I:
Experimen-
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