Title: Flight investigation at high mach numbers of several methods of measuring static pressure on an airplane wing
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003613532&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003613532&ix=nu&I=0&V=D&pm=1</a>
Subjects: Mach number, Bombers, Aerodynamics--Research.