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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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Separated Flow, NACA TN 3992, 1956.
41. Larson H. K., Heat Transfer in Separated Flows, J. Aeronaut. Sci..
, 26, № 11, pp. 731-738 (Nov. 1958).
42. С h a r w a t A. F., Dewey C. F., R о о s J. N.,
H i t г J. A..
Investigation of Separated Flows, Part II: Flow in the Cavity and Heat
Transfer, J. Aeronaut. Sci., 28, № 7, pp. 513-527 (July 1961).
43. G a d d G. E., Cope W. F., A t t г i d g с J. L., Heat
Transfer and
Skin-Fric.tion Measurements at a Mach Number of 2.44 for a
Turbulent
Boundary Layer on a Flat Surface and in Regions of Separated Flow, ARC R
& M 3148 (Oct. 1958).
b-0507
66
ГЛАВА I
44. С li u n g P. М., V i e g a s J. R., Heat Transfer at the
Reattachment Zone of Separated Laminar Roundary Layers, NASA TN D-1071
(Sept. 1961).
45. N a у s m i t h A., Heat Transfer and Boundary Layer Measurements in
a Region of Supersonic Flow Separation and Reattachment, ARC 20601, May
1958.
46. Coles D., .The Law of the Wake of the Turbulent Boundary Layer, J.
Fluid Mech., 1, Part 2, pp. 191 - 226 (July 1956).
47. T h о m a n n H., Measurements of Heat Transfer and Recovery
Temperature in Regions of Separated Flow at Mach Number 1.8, Aeronautical
Research Institute of Sweden, Rept 82, 1959.
48. R о s h к о A., On the Wake and Drag of Bluff Bodies, /. Aeronaut.
Sci., 22, № 2, pp. 124-132 (Feb. 1955).
49. К a v a n a u L. L., Base Pressure Studies in Rarefied Supersonic
Flows, J. Aeronaut. Sci., 23, № 3, pp. 193-230 (March 1956).
50. M a i r W. A., Experiments on Separation of Boundary Layers on Probes
in Front of Blunt Nosed Bodies in a Supersonic Air Stream, Phil. Mag.,
43, 7th series (July 1952).
51. Moeckel W. E., Flow Separation Ahead of Blunt Bodies at Supersonic
Speeds, NACA TN 2418 (July 1951).
52. С h a p m a n D. R., An Analysis of Base Pressure at Supersonic
Velocities and Comparison with Experiment, NACA TN 2137 (July 1950).
53. В о g d о n о f f S. М., A Preliminary Study of Reynolds Number
Effects on Base Pressure at M = 2.95, J. Aeronaut. Sci., 19, № 3 (March
1952).
54. С h a p m a n D. R., Wimbrow W. R., К e s t e r R. H., Experimental
Investigation of Base Pressure on Blunt Trailing Edge Wings at Supersonic
Velocities, NACA TN 2611.
БИБЛИОГРАФИЯ
Abbott D. E., Holt М., Nielsen J. N., Investigation of Hypersonic Flow
Separation and Its Effects on Aerodynamic Control Characteristics, Flight
Control Lab., Aeronautical Systems Div., Wright-Patterson Air Force Base,
Ohio, ASD-TDR-62-963, Nov. 1962.
Amick J.L., A Semiempirical Relation for Laminar Separation J. A erol
Space Sci., (Sept. 1959).
Chang P. K., Research on Flow Separation in Western Europe, US Air
Force., Office of Scientific Research, Washington, DC, AFOSR 4854, the
Catholic University of America, July 1963.
Cooke J. C., Hall M. G., Boundary Layers in Three Dimensions, Progress in
Aeronautical Sciences, Vol. 2, Pergamon Press.
F r a e n к e 1 L. E., On Corner Eddies in Plane Inviscid Shear Flow, J.
Fluid Mech., 11, Part 3, pp. 400-406 (Nov. 1961).
Friberg E. G., Measurement of Vortex Separation, Part I: Two-dimensional
Circular and Elliptic Bodies, Massachusetts Institute of Technology,
Technical Report 114, Aug. 1965.
Friberg E. G., Measurement of Vortex Separation, Part II: Three-
dimensional Circular,and Elliptic Bodies, Massachusetts Institute of
Technology, Technical Report 115, Aug. 1965.
Fung Y. C., Fluctuating Lift and Drag Acting on a Cylinder in a Flow at
Supercritical Reynolds Numbers, Space Technology Labs, Division of the
Thompson Ramo-Wooldridge Corp., EM 8-5, May 1958.
Grove A. S., Shair F. H., Petersen E. E., Acrivos A., An Experimental
Investigation of the Steady Separated Flow Past a Circular Cylinder, J.
Fluid Mech., 19, Part 1 (May 1964).
Harper J. F., On Boundary Layers in Two-dimensional Flow with Vortici-ty,
J. Fluid Mech., 17, Part. 1, pp. 141-153 (Sept. 1963).
ВВЕДЕНИЕ В ПРОБЛЕМЫ ОТРЫВА ПОТОПА
67
Haworth D. К., Р о tors А. R., Analytical Investigations of Laminar
Separations Using the "Crocco- Lees Mixing Parameter" Method, NASA
Contractor Rept 745 (May 1967).
X e й з e p, Влияние магнитных пилен на отрыв, Ракетная техника и
космонавтика, Л" 12 (1964).
Kaufman L. G., И, М е с к 1 е г L., Hai-tofil is S. A., An Investigation
of Flow Separation and Aerodynamic Controls at Hypersonic Speeds, AIAA
Paper Л; 65-752, Nov. 15-18, 1965.
Kline S. J., Dean R. C., Jr.. Unsolved Problems of Fluid Mechanics, Mech.
Engng, 80, Л" 12 (Dec. 1958).
К о r s t H. II., Dynamics and Thermodynamics of Separated Flows,
presented at the Symposium on Single- and Multi-component Flow Processes,
May 1, 1964, Rutgers Engineering Centennial, Rutgers, the State
University.
Murphy J. S., The Separation of Axially Symmetric Turbulent Boundary
Layers. Part II: Detailed Measurements in the Boundary Layers on Several
Slender Bodies in Incompressible Flow, Douglas Aircraft Division, Long
Beach, Calif., Rept Ns ES 17513 (Aug. 1955).
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