Hydrodynamic inertia coefficients for a slender body with a sail
Authors:
Theodore R. Goodman and Ralph Greif
Journal:
Quart. Appl. Math. 19 (1961), 137-141
MSC:
Primary 76.99
DOI:
https://doi.org/10.1090/qam/128741
MathSciNet review:
128741
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H. Lamb, Hydrodynamics, 6th ed., Dover, New York, 1932, Chap. VI
M. M. Munk, The aerodynamic forces on airship hulls, N. A. C. A. Report No. 184, 1924
- Robert T. Jones, Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound, Tech. Rep. Nat. Adv. Comm. Aeronaut. 1946 (1946), no. 835, 5. MR 35155
J. R. Spreiter, The aerodynamic forces on slender plane and cruciform wing and body combinations, N. A. C. A. Report No. 962, 1950
A. E. Bryson, Stability derivatives for a slender missile with application to a wing-body-vertical-tail configuration, J. Aeronaut. Sci. 20, No. 5, 297 (May 1953)
R. G. Summers, On determining the additional apparent mass of a wing-body-vertical-tail cross section, Readers’ Forum, J. Aeronaut. Sci. 20, No. 12, 856 (Dec. 1953)
A. E. Bryson, Comment on the stability derivatives of a wing-body-vertical-tail configuration, Readers’ Forum, J. Aeronaut. Sci. 21, No. 1, 59 (Jan. 1954)
- John W. Miles, The potential theory of unsteady supersonic flow, Cambridge Monographs on Mechanics and Applied Mathematics, Cambridge University Press, New York, 1959. MR 0102312
A. E. Bryson, Evaluation of the inertia coefficients of the cross section of a slender body, Reader’s Forum, J. Aeronaut. Sci. 21, No. 6, 424 (June 1954)
H. Lamb, Hydrodynamics, 6th ed., Dover, New York, 1932, Chap. VI
M. M. Munk, The aerodynamic forces on airship hulls, N. A. C. A. Report No. 184, 1924
R. T. Jones, Properties of low aspect ratio pointed wings at speeds below and above the speed of sound, N. A. C. A. Report No. 835, 1946
J. R. Spreiter, The aerodynamic forces on slender plane and cruciform wing and body combinations, N. A. C. A. Report No. 962, 1950
A. E. Bryson, Stability derivatives for a slender missile with application to a wing-body-vertical-tail configuration, J. Aeronaut. Sci. 20, No. 5, 297 (May 1953)
R. G. Summers, On determining the additional apparent mass of a wing-body-vertical-tail cross section, Readers’ Forum, J. Aeronaut. Sci. 20, No. 12, 856 (Dec. 1953)
A. E. Bryson, Comment on the stability derivatives of a wing-body-vertical-tail configuration, Readers’ Forum, J. Aeronaut. Sci. 21, No. 1, 59 (Jan. 1954)
J. W. Miles, The potential theory of unsteady supersonic flow, Cambridge University Press, 1959, p. 171
A. E. Bryson, Evaluation of the inertia coefficients of the cross section of a slender body, Reader’s Forum, J. Aeronaut. Sci. 21, No. 6, 424 (June 1954)
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Article copyright:
© Copyright 1961
American Mathematical Society