Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 /

Chicago citation style
Mack, Robert J. Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 /. 1974. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444471. (Accessed November 16, 2018.)
APA citation style
Mack, Robert J, (1974) Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6 /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444471
MLA citation style
Mack, Robert J. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444471>.
Note: These citations are programmatically generated and may be incomplete.