Effect of Compressibility on Normal-force, Pressure, and Load Characteristics of a Tapered Wing of NACA 66-series Airfoil Sections with Split Flaps
1948-12-01
Sonstige
Keine Angabe
Englisch
EFFECT OF COMPRESSIBILITY , AIRFOILS - NACA 66-SERIES (A=0 6) - ORDINATES - LOW-DRAG , WING FLAPS, SPLIT , WIND TUNNEL TESTS - NACA - HIGH-SPEED (16') WORK CARRIED ON AT LAL , PRESSURE DISTRIBUTION - AIRFOILS - NACA 66-SERIES , WINGS, TAPERED - CHARACTERISTICS , WING FLAPS, SPLIT - FULL-SPAN VS PARTIAL-SPAN , PITCHING MOMENTS - WINGS, TAPERED
Engineering Index Backfile | 1948
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