Numerical evaluation of the wake-survey equations for subsonic flow including the effect of energy addition
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1945
Place of publication: Langley Field, VA
Language: eng
Number of pages: 94
Subjects: Wakes (Aerodynamics; Aeronautics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003624211&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003624211&ix=nu&I=0&V=D&pm=1</a>