Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight
Publisher: NACA
Published: 1953
Place of publication: Washington, D.C.
Language: eng
Number of pages: 22
Subjects: Airplanes--Wings, Triangular; Fighter planes--Wings--Testing; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1</a>