Design and calibration of a nozzle to give a Mach number of 1.2 in the test section of the Cornell Aeronautical Laboratory 12-foot variable density wind tunnel
By: Seymour J. Weitchman.
Contributors: Cornell Aeronautical Laboratory
Series: Cornell Aeronautical Laboratory. Report -- no. 510,286-1
Publisher: Cornell Aeronautical Laboratory
Published: 1950
Place of publication: Buffalo, N.Y
Notes: Bibliographical references: p. 8.