Theoretical investigation of the drag of generalized aircraft configurations in supersonic flow
Publisher: NACA
Published: 1957
Place of publication: Washington, D.C.
Language: eng
Number of pages: 120
Subjects: Drag (Aerodynamics; Aerodynamics, Supersonic; Airplanes--Design and construction.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1</a>