SLENDER-BODY THEORY - REVIEW AND EXTENSION

[1] ON AN EXTENSION OF SLENDER-WING THEORY [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (06): : 424 - 425

[2] ALLEN H, 1950, NACA TN2044

[3] SUPERSONIC FLOW ROUND POINTED BODIES OF REVOLUTION [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1949, 2 (01) : 98 - 120

[4] DWIGHT HB, 1934, TABLES INTEGRALS OTH

[5] ELLIS MC, 1949, NACA TN1955

[6] FLAX AH, 1951, 3RD P ANGL AM AER C, P363

[7] GRAHAM EW, 1949, SM13417 DOUGL AIRCR

[8] ON HYPERSONIC SIMILITUDE [J]. QUARTERLY OF APPLIED MATHEMATICS, 1947, 5 (01) : 105 - 106

[9] HEASLET MA, 1950, NACA956 REP

[10] HEASLET MA, 1949, NACA TN1824

[1] ON AN EXTENSION OF SLENDER-WING THEORY [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (06): : 424 - 425

[2] ALLEN H, 1950, NACA TN2044

[3] SUPERSONIC FLOW ROUND POINTED BODIES OF REVOLUTION [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1949, 2 (01) : 98 - 120

[4] DWIGHT HB, 1934, TABLES INTEGRALS OTH

[5] ELLIS MC, 1949, NACA TN1955

[6] FLAX AH, 1951, 3RD P ANGL AM AER C, P363

[7] GRAHAM EW, 1949, SM13417 DOUGL AIRCR

[8] ON HYPERSONIC SIMILITUDE [J]. QUARTERLY OF APPLIED MATHEMATICS, 1947, 5 (01) : 105 - 106

[9] HEASLET MA, 1950, NACA956 REP

[10] HEASLET MA, 1949, NACA TN1824