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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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Leitflachen, Forsch. Geb. IngWes., 5, pp. 105-117 (May - June 1934).
56. Demontis J., Recherches sur 1'influence de l'angle d'ouverture d'un
ajutage divergent sur l'ecoulement a deux dimensions de Fair a travers
cet ajutage, Pub. Sci. et Tech. du Ministere de Fair, № 87, 1936.
57. Sorensen E., Wandrauhigkeitseinfluss bei Stromungsmaschinen,
Forsch.Geb. IngWes., 8, p. 25 (1937).
58. P о 1 z i n J., Der Einfluss der Wandrauhigkeit bei
Stromungsmaschinen, VDI - Zeitschrift, 81, p. 531 (1937), № 18, pp. 521 -
522.
59. Young A. D., Green G. L., TesSs of High-speed Flow in Diffusers of
Rectangular Cross-section, RM, № 2201, ARC, 1944.
60. Squire H. B., Carter P., Further Experiments on Conical Diffusers,
ARC Rept, № 13, 499 (British NPL Rept NV TP 320), Nov.
1950.
61. V о n R u с h t i O., Research on Radial Diffusers, Bericht der
Deuts-chen Forschungsanstalt fur Segelflug, Ernst Udet fnstitut fur
Aerodynamik und Flugmechanik, Technische Berichte, Vol. 11, 1944.
62. В i e b e 1 W. J., Low-pressure Boundary-Layer Control in Diffusers
and Bends, NACA WR L-84, 1945 (formerly NACA ARR 15C24).
63. К a 1 i n s k e A. A., Conversion of Kinetic Energy to Potential
Energy in Flow Expansion, Trans. Am. Soc. Civ. Engrs, 3, pp. 355-390
(1946).
64. Гуржиенко Г. А. Об установившемся турбулентном течении в коническом
диффузоре с малым углом раствора. Труды ЦАГИ, вып. 462, 1939.
65. Gratzer L. В., Smith R. Н., Boundary Layer Control for Wide Angle
Diffusers, Univ. of Washington Aeronautical Laboratory Rept, № 300 (Nov.
1948).
66. Robertson J. М., Ross D., Water Tunnel Diffuser Flow Studies, Part
11, Experimental Research, Penn. State College (July 1949).
67. Nelson W. J., Popp E. G., Performance Characteristics of Two 6° and
Two 12° Diffusers at High Flow Rates, NACA RM L9H09, Jan. 1952.
68. Wood С. C., Preliminary Investigations of the Rectangular Vortex
Generators on the Performance of a Short 1.9:1 Straight Wall Annular
Diffuser, NACA RM L51G09, 1951.
69. Martin R. C., Effects of Inlet Wall Contour on the Pressure Recovery
of a 10° 10-inch Inlet Diameter Conical Diffuser, NACA RM L-51 Ella,
1951.
70. P e r s h J., The Effect of Surface Roughness on the Performance of a
23° Conical Diffuser at Subsonic Mach Numbers, NACA RM L-51 K09, Jan.
1952.
71. V a 1 e n t i n e E. F., Carroll R. B., Effects of Some Preliminary
Variables of Rectangular Vnrlex Generators in the Static Pressure Rise
Through a Short Diffuser, NACA RM L-52B13, 1952.
72. К 1 i n e S. J., R u n s t a 1 d e г P. W. Some Preliminary Results
of Visual Studies on the Flow Model of the Wall Layers of the Turbulent
ОТРЫВ ТУРБУЛЕНТНОГО ПОТОКА ЖИДКОСТИ
207
Boundary Layer, J. Appl. Mech., 26, Trans. ASME, 81, pp. 166-170 (1953).
73. Squire H. B., Experiments on Conical Diffusers, Ministry of Supply,
ARC RM, № 2751, 1953.
74. L i t t 1 e В. H., Jr., Wilbur S. W., Performance and Boundary Layer
Data from 120° and 23° Conical Diffusers of Area Ratio 2,0 at Mach
Numbers up to Choking and Reynolds Numbers up to 7, 5 x 106, NACA Rept
1201, 1954. (Supersedes NACA RM L9H10 by Copp and Kle-vath; RM L9K10 by
Persh; RM L50C02a by Little and Wilbur.)
75. Бам-Зеликович Г. М., Расчет отрыва пограничного слоя Изв. АН СССР,
ОТН, № 12 (1954).
76. Р е г s h J., Bailey В. М., Effect of Surface Roughness over the
Downstream Region of a 23° Conical Diffuser, NACA TN 3066. 1954.
77. F a u 1 d e r s C. R., Aerodynamic Design of Vaned Diffusers for
Centrifugal Compressors, ASME Paper, № 56-A213, 1956.
78. Halzhauser C. A., Hall L. P., Exploratory Investigation of the Use of
Area Suction to Eliminate Air Flow Separation in Diffusers having Large
Expansion Angles, NACA TN 3793, Oct. 1956.
79. Scott - Wilson J. B., Llewelyn-Davis D. I. T. P., The Development of
an Improved Diffuser for the 3 ft x 3 ft Tunnel, RAE Tech. Note Aero.
2446, July 1956.
80. Scherrer R., Anderson S. E., Preliminary Investigation of a Family of
Diffusers Designed for Near Sonic Inlet Velocities, NACA TN 3668, 1956.
81. W о о 1 1 e t t R. R., Preliminary Investigation of Short Two-
dimensio nal Subsonic Diffusers, NACA RM E56C02 (May 1956).
82. N о г b u г у J. F., Some Measurements of Boundary Layer Growth in a
Two-dimensional Diffuser, J. Basic Engng, Trans. ASME, Ser. D, 81. pp.
285-296 (1959).
83. Gauger М., диссертация Technische Hochschule, Breslau, 1934.
84. Schlichting H., Application of Boundary Layer Theory in Turbo-
Machinery, J., Basic Engng, Trans ASME (Dec. 1959).
85. К 1 i n e S. J., A b о t t D. E., Fox R. W., Optimum Design of
Straight-walled Diffusers, J. Basic Engng, Ser D. pp. 321-331 (Sept.
1959).
86. Johnston J. P., The Three-dimensional Turbulent Boundary Layer, MIT
Gas Turbine Laboratory Rept 39, May 1957 (or ASME Paper 59-HYD-6), J.
Basic Engng, Ser. D. pp. 622-628 (Sept. 1960).
87. Maskell E. C., Flow Separation in Three-dimensions, Rept № Aero.
2565, Royal Aircraft Establishment, Farnborough (Nov. 1955).
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