Effect of convergent ejector nozzles on the boattail drag of a 16° conical afterbody at Mach number of 0.6 to 1.26 /
by James M. Cubbage, Jr.
APA Citation
Cubbage, J. M., United States. National Adviosry Committee for Aeronautics., Langley Aeronautical Laboratory. (1958). Effect of convergent ejector nozzles on the boattail drag of a 16° conical afterbody at Mach number of 0.6 to 1.26. Washington, D.C.: National Advisory Committee for Aeronautics.
MLA Citation
Cubbage, James M, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory. Effect of Convergent Ejector Nozzles On the Boattail Drag of a 16° Conical Afterbody At Mach Number of 0.6 to 1.26. Washington, D.C.: National Advisory Committee for Aeronautics, 1958.
Warning: These citations may not always be complete (especially for serials).