Title: Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638560&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638560&ix=nu&I=0&V=D&pm=1</a>
Subjects: Airplanes--Wings, Aerofoils, Aerodynamics--Research.