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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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edge Separation, NACA Tech. Note 3430, April 1955; см. также J. Aeronaut.
Sci., 21, pp. 690-694, 706 (1954).
42. Mac Adams C., Leading-edge Separation from Delta Wings at Supersonic
Speeds, /. Aeronaut. Sci., 29, pp. 430, 1953.
43. Alexander A. J., Experimental Investigation on a Cropped Delta Wing
with Edge Blowing, College of Aeronautics Rept, № 162, ARC 25213, June
1963.
44. Alexander A. J., Experiments on a Delta Wing Using Leading-edge
Blowing to Remove the Secondary Separation, College of Aeronautics Rept,
№ 161, May 1963.
45. В e r g e n s e n A. J., Porter J. D., An Investigation of the Flow
Around Slender Delta Wings with Leading-edge Separation, Princeton Univ.,
Aero Engng Dept., Rept № 510, May 1960.
46. D о r e B. D., Non-linear Theory for Slender Wings in Sudden Plunging
Motion, NPL Aero. Rept 1128, ARC 26488, Dec. 1964.
47. Earnshaw P. B., An Experimental Investigation of the Structure of a
Leading-edge Vortex, ARC R & M 3281, 1961.
48. Edwards R. H., Leading-edge Separation from Delta Wings, J. Aeronaut.
Sci., 21, pp. 134-135, 1954.
49. F i n k P. Т., Taylor J., Some Low-speed Experiments with 20 Degree
Delta Wings, Imperial College, Dept, of Aeronautics, ARC 17854, Sept.
1955.
50. Garner H. C., Lehrian D. E., Non-linear Theory of Steady Forces on
Wings with Leading-edge Flow Separation, NPL Aero, Rept 1059, ARC R & M
3375, 1963.
51. Gersten K., Nichtlineare Tragflachentheorie insbesondere fiir Trag-
fliigel mit kleinem Seitenverhaltnis, Ing.-Archiv, 30, pp. 431-452
(1961).
52. Gregory N., Love E. М., Some Problems of Flow Laminarization on a
Slender Delta Wing, NPL Aero. Rept 1138, ARC 26754, Feb.
1965.
53. Hall M. G., A Theory for the Core of a Leading-edge Vortex, J. Fluid
Mech., 11, pp. 209-228 (1961).
ОТРЫВ ЛАМИНАРН. ПОТОКА ЖИДКОСТИ НА ПРОСТРАН. ТЕЛАХ 139
54. Hummel D., Experimentelle Untersuchung der Stromung auf der Saug-
seite eines schlanken Delta Fliigels, Z. Flugwiss., 13, pp. 247-252
(1965).
55. Kiichemann D., A Non-linear Lifting Surface Theory for Wings of Small
Aspect Ratio with Edge Separations, RAE Rept Aero. 2540, ARC 17769, April
1955.
56. L a m b о u r n e H. С., В г у e r D. W., Some Measurements in the
Vortex Flow Generated by a Sharp Leading-edge having 65° Sweep, ARC
21073, 1959.
57. L a w f о r d J. A., Low-specd Wind Tunnel Experiments on a Series of
Sharp-edged Delta Wings. Part II: Surface Flow Patterns and Boundary
Layer Transition Measurements, RAE Tech. Note Aero. 2954, ARC 26032,
March 1964.
58. Legendre R., ficoulement au voisinage de la pointe avant d'une aile a
forte fleche, Rech. aero., № 35 (1953).
59. Legendre R., ficoulement au voisinage de la pointe avant d'une aile a
forte fleche aux incidences moyennes, 8th Int. Cong. Th. Appl. Mech.,
Instanbul 1952, Rech. aero., № 30 (1952), № 31 (1953).
60. L о w s о n W. V., The Separated Flows on Slender Wings in Unsteady
Motion, Dept, of Aeronautics and Astronautics, Univ. of Southampton, Rept
ARC 25118, Sept. 1963.
61. M a s к e 1 1 E. C., On the Asymptotic Structure of a Conical
Leading-edge Vortex, presented to IUTAM Symposium on Concentrated Vortex
Motions, Ann Arbor, July 1964.
62. P e с к h am D. H., Low Speed Wind-tunnel Tests on a Series of
Uncambered Slender Pointed Wings with Sharp Edges, RAE Rept № Aero. 2613
ARC R & M 3186, Dec. 1958.
63. Rainbird W. J., С г a b b e R. S., P e a к e D. J., M e у e г R. F.,
Some Examples of Separation in Three-dimensional Flows, Quart. Bull. Div.
Mech. Engng Nat. Aeronaut. Establ. Can.', National Research Council of
Canada, Rept № DME/NAE, 1966 (1), Jan.- March 1966.
64. R a n d a 1 1 D. G., An Attempt to Predict the Effects of Leading-
edge Separation Without the Assumptions of Slender Wing Theory, RAE (ne-
опубликовано).
65. Randall D. G., Oscillating Slender Wings in the Presence of Leading-
edge Separation, RAE Rept № Struct. 286, ARC 24939, April 1963.
66. R a n d a 1 1 D. G., A Theoretical Determination of the Flow Past and
the Air Forces on an Oscillating Slender Delta Wing with Leading-edge
Separation, RAE Rept № Struct. 280, ARC 24910, March 1963.
67. R 0 t t N., Diffraction of a Weak Shock with Vortex Generation, J.
Fluid Mech., 1, pp. Ill-123 (1956).
68. Roy М., Caracteres de l'ecoulement autour d'une aile en fleche
accentuee, CR Acad. Sci. Paris, 234, pp. 2501 (1952).
69. Roy М., On the Rolling-up of the Conical Vortex Sheets from a Delta
Wing, presented to IUTAM, Symposium on Concentrated Vortex Motions, Ann
Arbor, July 1964, Prog, in Aeron. Sci., ed. Kiichemann etal., Vol. 7,
Pergamon Press, Oxford, 1966,
70. S m i t h J. H. B., Theoretical Work on the Formation of Vortex
Sheets, Prog, in Aeron. Sci., ed. Kiichemann et al., Vol. 7, Pergamon
Press, Oxford,
1966.
71. Smith J. H. B., A Theory of the Separated Flow from the Curved
Leading-edge of a Slender Wing, ARC R & M 3116, 1957.
72. S q u i r e L. C., The Estimation of the Non-linear Lift of Delta
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