Отрывные течения. Том 3 - Чжен П.
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ТЕПЛОВЫЕ ЯВЛЕНИЯ В ОТРЫВНЫХ ТЕЧЕНИЯХ
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Transfer and Fluid Mechanics Institute, 1958, and Princeton
University, Aero. Eng. Dept. Rept 412, March 1958.
78. Crawford D. H., Investigation of the Flow Over a Spiked-nose He-
misphere-cylinder at a Mach Number of 6.8, NASA TN D-118, Dec. 1959.
79. W о о d С. J., A Study of Hypersonic Separated Flows, doctoral
thesis, University of London, Oct. 1961.
80. F a g e A., Experiments on a Sphere at Critical Reynolds Numbers, ARC
R & M, № 1766, 1937.
81. Sti.ne H. A., Wanlass K., Theoretical and Experimental Investigation
of Aerodynamic Heating and Isothermal Heat-transfer Parameters on a
Hemispherical Nose with Laminar Boundary Layers at Supersonic Mach
Numbers, NACA TN 3344, 1954.
82. С о h e n N. B., A Method for Computing Turbulent Heat Transfer in
the Presence of Streamwise Pressure Gradient for Bodies of High-speed
Flow, NASA Memo. 1-2-592, 1959.
83. Powers W. E., Stetson K. F., Adams М. C., A Shock Tube Investigation
of Heat Transfer in the Wake of a Hemisphere Cylinder with Application to
Hypersonic Flight, AVCO Research Laboratory, Rept 30, Aug. 1958.
84. Rabinowicz J., Measurements of Turbulent Heat Transfer Rates on the
Aftportion and Blunt Bodies of Hemisphere Cylinder in the Shock Tube,
GALCIT Hypersonic Research Project Memo. 41, 1957.
85. Chung P. М., Viegas J. R., Heat Transfer at the Reattachment Zone of
Separated Laminar Boundary Layers, NASA TN D-1072, Sept. 1961.
86. Lees L., Laminar Heat Transfer Over Blunt-nosed Bodies at Hypersonic
Flight Speeds, Jet Propulsion, 26, № 4, 259-269, 274 (April 1956).
87. Chapman D. R., К u e h n D. М., Larson H. K., Investigation of
Separated Flows in Supersonic and Subsonic Streams with Emphasis on the
Effect of Transition, NACA TN 3869, 1957.
88. Николь, Исследование ламинарного гиперзвукового течения в выемке,
Ракетная техника и космонавтика, № 9, стр. 21 (1964).
89. Chapman D. R., Laminar Mixing of a Compressible Fluid, NACA Rept 958,
1950.
90. Chapman D. R., Rubesin M. W., Temperature and Velocity
Profiles in the Compressible Laminar Boundary Layer with Arbitrary
Distribution of Surface Temperature, J. Aeronaut. Sci., 16, № 9, 547-565
(Sept. 1949). '
91. Bloom М., Boundary Layers with Variable Heat Capacity on Noniso-
thermal Surfaces, J. Aeronaut. Sci., 20, № 10, 719 (Oct. 1953).
92. С u r 1 e N., The Effects of Heat Transfer on Laminar Boundary Layer
Separation in Supersonic Flow, ARC TM 2956, May 1960.
93. Carlson W. O., Heat Transfer in Laminar Separated and Wake Flow
Regions, Paper presented at 1959 Heat Transfer and Fluid Mechanics
Institute held at University of California, Los Angeles, Stanford
University Press, Stanford. California. June 1959, p. 140-155.
94. Bloom М. H-, P a 1 1 о n e A., Shroud Tests of Pressure and Heat
Transfer Over Short Afterbodies with Separated Wakes, WADC TN 58-185,
Polytechnic Institute of Brooklyn, June 1958.
95. С h a p m a n D. R., An Analysis of Base Pressure at Supersonic
Velocities and Comparison with Experiment, NACA TR 1051, 1951.
96. Walz A., Beitrag zur Naherungstheorie kompressibler turbulenter
Grenz-schichten, DVL Rept, № 84, 1959.
БИБЛИОГРАФИЯ
В atche 1 о r G. К., Heat Transfer by Free Convection across a Closed
Cavity between Vertical Boundaries at Different Temperatures, Ouart AddI
Math., 12, № 3, 209- 233 (Oct. 1954).
198
ГЛАВА XI
Burchfield С. G.,Hube F. К.,Burdette J. E., An Experimental Heat-
transfer Investigation in Regions of Flow Separation at Mach Number 8,
Tech. Documentary Rept № AEDC-TDR-64-30, Feb. 1964.
Carlson W. O., A Solution for Heat Transfer in Laminar Separated and
Wake Flow Regions, R59SD356, ASTIA, 1959.
Chang P. K., N о 11 a g e H. B., Prediction of Local Skin-friction
Coefficient by Transformation of the Compressible Boundary Layer with
Heat Transfer, J. Franklin Inst., 271, № 6 (June 1961).
Cole D., Brainerd J. J., Slender Wings at High Angles of Attack in
Hypersonic Flow, American Rocket Society, Air Force Office of Scientific
Research, International Hypersonics Conf., Aug. 1961, MIT.
F a n d R. М., R о о s ]., Cheng P., Kaye J., The Local Heat-transfer
Coefficient Around a Heated Horizontal Cylinder in an Intense Sound
Field, ASME Paper № 61-WA-172.
F i 1 e 11 i E. G-, Experimental Investigation of Heat Transfer in the
Stall Region Behind a Double Backward Facing Step (диссертация), Nov.
1965.
Fox J., Heat Transfer and Air Flow in a Transverse Rectangular Notch,
Int. J. Heat Mass Transfer, 8, № 2, 269-279 (Feb. 1965).
Furey R. J., Heat Transfer in Regions of Separated Flow Induced by
Surface Cavities (диссертация), May 1962.
G a d d G. E., An Experimental Investigation of Heat Transfer Effects on
Boundary Layer Separation in Supersonic Flow, J. Fluid Mech., 2, 105- 122
(1957).
Holloway P. F., Sterrett J. R., С г e e к m о r e H. S., An
