Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 18
Subjects: Yawing (Aerodynamics; Compressibility; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003638540&ix=nu&I=0&V=D&pm=1" rel="ugc nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003638540&ix=nu&I=0&V=D&pm=1</a>