Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1944
Place of publication: Langley Field, VA
Language: eng
Number of pages: 18
Subjects: Airplanes--Wings; Aerofoils; Aerodynamics--Research.
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>