Kehlet, Alan B.
Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]
/ Alen B. Kehlet
.- Washington, D.C.: Nasa, 1961
.- 26p .
.- ( National Aeronautics and Space Administration (NASA)
Subject Headings:
Aerodynamic;
Copy Details:
Acc. No.: TR16137, Full Call No.: NASA TN D-836, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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