THE SLENDER ELLIPTIC CONE AS A MODEL FOR NON-LINEAR SUPERSONIC FLOW THEORY

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VANDYKE, MD

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O3 [力学];

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08 ; 0801 ;

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页码：1 / 15

页数：15

共 19 条

[1] SLENDER-BODY THEORY - REVIEW AND EXTENSION
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[2] BROERICK JB, 1949, Q J MECH APPL MATH, V2, P98
[3] FENAIN M, 1955, CR HEBD ACAD SCI, V241, P276
[4] SUPERSONIC FLOW OVER CONICAL BODIES WITHOUT AXIAL SYMMETRY
FERRI, A
NESS, N
KAPLITA, TT
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (08): : 563 - 571
[5] FERRI A, 1951, 1102 NAT ADV COMM AE
[6] FRAENKEL LE, 1952, AERO RES COUN LOND R, V2954
[7] IMAI I, 1952, 1 P JAP NAT C APPL M, P349
[8] LEADING-EDGE SINGULARITIES IN THIN-AIRFOIL THEORY
JONES, RT
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (05): : 307 - 310
[9] Jones RT, 1946, 835 NAT ADV COMM AER
[10] SUPERSONIC FLOW ABOUT SLENDER BODIES OF ELLIPTIC CROSS SECTION
KAHANE, A
SOLARSKI, A
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (08): : 513 - 524