Vertical strut installation for testing sting-mounted models in the Cornell Aeronautical Laboratory, Inc. 8.5' by 12' variable density wind tunnelE. J. Lays · First published 1951Open the Tome
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 tunnelSeymour J. Weitchman · First published 1950Open the Tome
