Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction /

Chicago citation style
Wasserbauer, Joseph F. Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction /. 1969. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444615. (Accessed December 11, 2018.)
APA citation style
Wasserbauer, Joseph F, (1969) Dynamic response of a Mach 2.5 axisymmetric inlet with engine or cold pipe and utilizing 60 percent supersonic internal area contraction /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444615
MLA citation style
Wasserbauer, Joseph F. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444615>.
Note: These citations are programmatically generated and may be incomplete.