Exploratory Investigation at High and Low Subsonic Mach Numbers of Two Experimental 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients
1951-12-14
Sonstige
Keine Angabe
Englisch
Investigation of lifting 10-percent-thick symmetrical double-wedge airfoil at mach numbers up to 1
Engineering Index Backfile | 1954
|LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 13.1-PERCENT-THICK, HIGH-LIFT AIRFOIL*
SAE Technical Papers | 1974
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