Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0
Publisher: NACA
Published: 1954
Place of publication: Washington, D.C.
Language: eng
Number of pages: 24
Subjects: Body of revolution; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1</a>