Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

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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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  • [3] 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
  • [4] 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
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  • [6] Milomir M. Stanišić, On the acceleration potential function for non-steady motion of a delta-wing in supersonic flight, Bul. Inst. Politehn. Iasi (N.S.) 6 (10) (1960), no. 1–2, 49–60 (English, with Russian and Romanian summaries). MR 0138282
  • [7] 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 0116689, https://doi.org/10.1002/zamm.19600400903
  • [8] E. A. Krassilchtchikova, Method of integral equations in thin wing theory in compressible medium, 9th Intern. Congr. Appl. Mech., 3, 57-67 (1956)
  • [9] M. M. Stanišic, A remark concerning the vibration of a delta-wing in supersonic flight, J. Aero. Sci. 26, 679-680 (1959)
  • [10] V. A. Kovaleva, On the nonstationary motion of a wing with rectangular planform, J. Appl. Math. Mech. 23 (1959), 1476–1491. MR 0115457, https://doi.org/10.1016/0021-8928(59)90005-X
  • [11] 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 0144567, https://doi.org/10.1002/zamm.19610410903

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DOI: https://doi.org/10.1090/qam/142273
Article copyright: © Copyright 1962 American Mathematical Society


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