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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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2.4, Brit. RAE Rept Aero. 2569, 1956.
39. Wimbrow W. R., Effect of Base Bleed on the Base Pressure of Blunt
Trailing-edge Airfoils at Supersonic Speeds, NACA RM A54A07, 1954.
40. К о r s t H. H., Tripp W., The Pressure on a Blunt Trailing Edge
Separating Two-supersonic Two-dimensional Air Streams of Different Mach
Numbers and Stagnation Pressures, but Identical Stagnation Temperatures,
Paper presented at the Midwest Conferences on Solid and Fluid Mechanics,
University of Michigan, Ann Arbor, Michigan, April 1957.
41. Carriere P., Sirieix М., Facteurs d'influence du recolement d'un
ecoulement supersonique, Paper presented to 10th International Congress
of Applied Mechanics, Stresa, Sept. 1960, ONERA Memo Tech. 20, 1961.
42. Kirk F. N., An Approximate Theory of Base Pressure in Two-
dimensional Flow at Supersonic Speeds, RAE TN Aero 2377, March 1954,
Issued Dec. 1959.
43. Karashima K., Base Pressure on Two-dimensional Blunt Trailing-edge
Wings at Supersonic Velocities, Aeronautical Research Institute,
University of Tokyo, Rept № 368, Vol 27, № 8, Oct. 1961.
44. Gortler H., Berechnung von Aufgaben der freien Turbulenz auf Grund
eines neuen Naherungssatzes, Z. angew. Math. Mech., 22 (1942).
45. Reichardt H., Gesetzmassigkeiten der freien Turbulenz, VDI-For-
schungsheft 414, 1951.
ДОННОЕ ДАВЛЕНИЕ
85
46. Gooderum Р. В., Wood G. P., Brevoort M. J., Investigation with an
Interferometer of the Turbulent Mixing of a Supersonic Jet, NACA Rept №
963, 1950.
47. Schubauer G. B., Klebanoff P. S., Investigation ol Separation of the
Turbulent Boundary Layer, NACA TN 2133, 1950.
48. С h a p m a n D. R., Laminar Mixing of a Compressible Fluid, NACA TN
1800, 1950.
49. С h a p m a n D. R., A Theoretical Analysis of Heat Transfer in
Regions of Separated Flows, NACA TN 3792, 1956.
50. С h a p m a n 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.
51. Денисон, Баум, Сжимаемый свободный струйный пограничный слой с
ненулевой начальной толщиной, Ракетная техника и космонавтика, № 2
(1963).
52. Baum Е., King Н. Н., Denison М. R., Recent Studies of the Laminar
Base Flow Region, AIAA 1st Aerospace Science Meeting, N. Y., Preprint 64-
5, Jan. 1964.
53. N a s h J. F., An Analysis of Two-dimensional Turbulent Base Flow,
Including the Effect of the Approaching Boundary Layer, ARC R & M, №
3344, July 1.962.
54. V a n Hise V., Investigation of Variation in Base Pressure over the
Reynolds Number Range in which Wake Transition Occurs for Two-dimensional
Bodies at Mach Numbers from 1.95 to 2.92, NASA TN D-167, Nov. 1959.
55. S i r i e i x М., Pression de culot et processus de melange
turbulent en ecoulement supersonique plan, Recherche aeronaut, № 78, 13
(Sept.-Oct. 1960).
56. T h о m a n n H., Measurements of Heat Transfer and Recovery
Temperature in Regions of Separated Flow at a Mach Number of 1,8, FFA
Rept 82, Stockholm, 1959.
БИБЛИОГРАФИЯ
Baum E., Effect of Boundary-layer Distortion at Separation on the Laminar
Base Flow, Electro-Optical Systems Inc., Pasadena, Calif., EOS Research
Note № 16, Oct. 1963.
Баум E., Начальное развитие отрывного ламинарного струйного течения,
Ракетная техника и космонавтика, № 1 (1964).
Brown J., Turbulent Base Flow behind a Slender Supersonic Re-entry
Vehicle. General Electric Re-entry Systems Dept., 63SD849, May 1964.
В u tsko J. E., Prediction of the Subsonic Base Drag of
Hypersonic Reentry Vehicles, А1АД 3rd
Annual Meeting, Boston, Mass., Paper № 66-991,
Nov.-Dec. 1966.
Butsko J.E., Carter W. V., Herman W., Development
of Sub-
sonic Base Pressure Prediction Methods, Air Force Flight Dynamics
Lab.. AFFDL-TR-65-157, Vol. I, Sept. 1965.
Butsko J. E., Carter W. V., Herman W., Development
of Sub-
sonic Base Pressure Prediction Methods, Air Force Flight Dynamics
Lab., AFFDL-TR-65-157, Vol. II, Sept. 1965.
Carlson W. O., A Solution for Heat Transfer in Laminar Separated and Wake
Flow Regions, Missile and Space Vehicle Dept.,General Electric, №
R59SD356, March 1959.
Cassanto J. М., Ratio on Base Pressure, American Institute of Aeronautics
and Astronautics, Copyright 1965, Vol. 3, № 12.
86
ГЛАВА X
Chapman D. R., Reduction of Profile Drag at Supersonic Velocities by the
Use of Airfoil Sections having a Blunt Trailing Edge, NACA TN 3503, Sept.
1955.
Fail R., Lawford J. A., Eyre R.C.W., Low Speed Experiments on the Wake
Characteristics of Flat Plates Normal to an Airstream, RAE TN Aero. 2516,
ARC 19.958, FM 2652-0.1393, June 1957.
Francis W., Davey W. Т., Base Heating Experiments on Slender Cones in
Hypersonic Flow, IAS National Summer Meeting, Calif., Paper № 62-179,
June 1962.
Hastings R. C., Turbulent Flow Past Two-dimensional Bases in Supersonic
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