NASA Technical Note [NASA TN D-4909]: Effects of angle of attack and bluntness on the shock-layer properties of a 15 degree cone at a mach number of 10.6
/ Joseph W. Cleary
.- Washington: NASA, 1968
.- 38p .
.- ( National Aeronautics and Space Administration NASA Technical Note
Bound together NASA TN D-4900 to 4910 Bound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268
Subject Headings:
Aeronautics;
Aircraft -- Conical bodies -- Flow distribution;
Aircraft -- Shock layers -- Angle of attack and bluntness
Author Added Entry:
Cleary, Joseph W.;
Copy Details:
Acc. No.: TR13267, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D-4900 to 4910
------------------------- --------------------- ------ --------- ------- ------- --------- --------
Bound together NASA TN D-4900 to 4910 Bound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268
Subject Headings:
Aeronautics;
Aircraft -- Conical bodies -- Flow distribution;
Aircraft -- Shock layers -- Angle of attack and bluntness
Author Added Entry:
Cleary, Joseph W.;
Copy Details:
Acc. No.: TR13267, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D-4900 to 4910
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