Effect of Compressibility on the Distribution of Pressures over a Tapered Wing of NACA 230-series Airfoil Sections
1947-07-01
Miscellaneous
No indication
English
EFFECT OF COMPRESSIBILITY , PRESSURE DISTRIBUTION - AIRFOILS - NACA 233016-23009 , WIND TUNNEL TESTS - NACA - HIGH-SPEED (16') , AIRFOILS - ANGLE OF ATTACK , CHORDWISE , PRESSURE DISTRIBUTION - AIRFOILS - NACA 230-SERIES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23016-23009 , AIRPLANES, FIGHTER , WORK CARRIED ON AT LMAL , PRESSURE DISTRIBUTION - WINGS, TAPERED-EFFECT OF COMPRESSIBILITY
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1948
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