Lift Tests of a 0.1536c Thick Douglas Airfoil Section of NACA 7-Series Type Equipped with a Lateral-Control Device for Use with a Full-Span Double-Slotted Flap on the C-74 Airplane

Lift Tests of a 0.1536c Thick Douglas Airfoil Section of NACA 7-Series Type Equipped with a Lateral-Control Device for Use with a Full-Span Double-Slotted Flap on the C-74 Airplane

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Bibliographische Detailangaben
1. Verfasser: Rice, Fred J, Jr
Format: Report
Sprache:eng
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