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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**[1]**A. Busemann, Infinitesimale kegelige Überschallströmung, Schriften, Deutsche Akademie der Luftfahrtforschung,**3**, 1943**[2]**L. A. Galin,*Wing of rectangular form in supersonic flow*, P.M.M.**11, 165-475**(1947)**[3]**S. V. Falkovich,*Lift force of a wing of finite span*, P.M.M.**11**, 171-177 (1947) MR**0024748****[4]**J. W. Miles,*The potential theory of unsteady supersonic flow*, Cambridge Univ. Press, (1959) MR**0102312****[5]**J. W. Miles,*A note on supersonic wing integral equations in unsteady flow*, Aeron. Quarterly**3**, 294 (1951-52) MR**0049027****[6]**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) MR**0138282****[7]**M. M. Stanišić,*On the solution of an integral equation appearing in delta-wing theory*, ZAMM**40**, 397-415 (1960) MR**0116689****[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 unsteady motion of wing of a rectangular form*, P.M.M.**23**, 1030-1041 (1959) MR**0115457****[11]**M. M. Stanišić,*On the aerodynamic forces acting on a delta wing in supersonic flow with supersonic leading edges*, ZAMM**41**, 342-354 (1961) MR**0144567**

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DOI:
https://doi.org/10.1090/qam/142273

Article copyright:
© Copyright 1962
American Mathematical Society