Free-flight simulation of the testing of supersonic inlet diffusers in a free jet wind tunnel with 50% area ratio in the Mach number range from 1.5 to 3
By: Rudolf Hermann and Cheng-Ting Hsu.
Contributors: Hsu, Cheng-Ting.; Arnold Engineering Development Center
Publisher: Arnold Engineering Development Center, Air Research and Development Command, U.S. Air Force
Published: 1955
Place of publication: [Arnold Air Force Station, Tenn.]
Number of pages: 219
Notes: Contract number: AF-18(600)-338