Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls.
Part II.
Conical cabin configuration /
Louis G. Kaufman.

APA Citation

Kaufman, L. G.., United States. Air Force. Systems Command., Air Force Flight Dynamics Laboratory (U.S.)., Grumman Aircraft Engineering Corporation. (1964). Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force.

MLA Citation

Kaufman, Louis G., United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Pressure Measurements for Mach Five Flows Over Winged Re-entry Configurations With Aerodynamic Controls. Wright-Patterson Air Force Base, Ohio: Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964.

Warning: These citations may not always be complete (especially for serials).