1 Result #1: Calibration of 30° included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.51 [1968] Creators & Contributors: Vahl, Walter A.; Weirich, Robert L. +1 more E-Book Washington, D.C. : National Aeronautics and Space Administration, August 1968 NAS 1.14:D-4679 Loading... FIND IT Online Connect to online resource Check availability
2 Result #2: Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 [1968] Creators & Contributors: Weirich, Robert L.; Vahl, Walter A. +1 more E-Book Washington, D.C. : National Aeronautics and Space Administration, October 1968 NAS 1.14:D-4809 Loading... FIND IT Online Connect to online resource Check availability