On a theory for unsteady motion of rectangular wing in supersonic flow
Author:
Milomir M. Stanišić
Journal:
Quart. Appl. Math. 20 (1962), 231-240
MSC:
Primary 76.44
DOI:
https://doi.org/10.1090/qam/142273
MathSciNet review:
142273
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Additional Information
A. Busemann, Infinitesimale kegelige Überschallströmung, Schriften, Deutsche Akademie der Luftfahrtforschung, 3, 1943
L. A. Galin, Wing of rectangular form in supersonic flow, P.M.M. 11, 165–475 (1947)
- S. V. Falkovich, Lift force of a wing of finite span, Appl. Math. Mech. [Akad. Nauk SSSR. Prikl. Mat. Mech.] 11 (1947), 171–176 (Russian, with English summary). MR 0024748
- 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
- John W. Miles, A note on supersonic wing integral equations in unsteady flow, Aeronaut. Quart. 3 (1952), 294–296. MR 49027
- Milomir M. Stanišić, On the acceleration potential function for non-steady motion of a delta-wing in supersonic flight, Bul. Inst. Politehn. Iaşi (N.S.) 6(10) (1960), no. 1-2, 49–60 (English, with Romanian and Russian summaries). MR 138282
- Milomir M. Stanišić, On the solution of an integral equation appearing in the delta-wing theory, Z. Angew. Math. Mech. 40 (1960), 397–414 (English, with German and Russian summaries). MR 116689, DOI https://doi.org/10.1002/zamm.19600400903
E. A. Krassilchtchikova, Method of integral equations in thin wing theory in compressible medium, 9th Intern. Congr. Appl. Mech., 3, 57–67 (1956)
M. M. Stanišic, A remark concerning the vibration of a delta-wing in supersonic flight, J. Aero. Sci. 26, 679–680 (1959)
- V. A. Kovaleva, On the nonstationary motion of a wing with rectangular planform, J. Appl. Math. Mech. 23 (1959), 1476–1491. MR 0115457, DOI https://doi.org/10.1016/0021-8928%2859%2990005-X
- Milomir Stanišić, On the aerodynamic forces acting on a delta-wing in supersonicflow with supersonic leading edges, Z. Angew. Math. Mech. 41 (1961), 342–354 (English, with German and Russian summaries). MR 144567, DOI https://doi.org/10.1002/zamm.19610410903
A. Busemann, Infinitesimale kegelige Überschallströmung, Schriften, Deutsche Akademie der Luftfahrtforschung, 3, 1943
L. A. Galin, Wing of rectangular form in supersonic flow, P.M.M. 11, 165–475 (1947)
S. V. Falkovich, Lift force of a wing of finite span, P.M.M. 11, 171–177 (1947)
J. W. Miles, The potential theory of unsteady supersonic flow, Cambridge Univ. Press, (1959)
J. W. Miles, A note on supersonic wing integral equations in unsteady flow, Aeron. Quarterly 3, 294 (1951-52)
M. M. Stanišić, On the acceleration potential function for nonsteady motion of a delta-wing in supersonic flight, Bulet. Inst. Polit. Iasi, (6) 10, 49–61 (1960)
M. M. Stanišić, On the solution of an integral equation appearing in delta-wing theory, ZAMM 40, 397–415 (1960)
E. A. Krassilchtchikova, Method of integral equations in thin wing theory in compressible medium, 9th Intern. Congr. Appl. Mech., 3, 57–67 (1956)
M. M. Stanišic, A remark concerning the vibration of a delta-wing in supersonic flight, J. Aero. Sci. 26, 679–680 (1959)
V. A. Kovaleva, On the unsteady motion of wing of a rectangular form, P.M.M. 23, 1030–1041 (1959)
M. M. Stanišić, On the aerodynamic forces acting on a delta wing in supersonic flow with supersonic leading edges, ZAMM 41, 342–354 (1961)
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Article copyright:
© Copyright 1962
American Mathematical Society
