TY  - BOOK
AU  - Cleary, Joseph W.
ED  - Washington. National Aeronautics and Space Administration (NASA)
TI  - 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
PY  - 1968///
CY  - Washington
PB  - NASA
KW  - Aeronautics
KW  - Aircraft -- Conical bodies -- Flow distribution
KW  - Aircraft -- Shock layers -- Angle of attack and bluntness
N1  - Bound together NASA TN D-4900 to 4910; Bound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268
ER  -