Title: Experimental pressure distributions over two wing-body combinations at Mach number 1.9
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003810661&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003810661&ix=nu&I=0&V=D&pm=1</a>
Subjects: Airplanes--Wings, Aerodynamics--Research.