Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1946
Place of publication: Langley Field, VA
Language: eng
Number of pages: 64
Subjects: Parachutes; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003616345&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003616345&ix=nu&I=0&V=D&pm=1</a>