A reference for engineers and students, this volume devotes more than 300 pages to theoretical and experimental considerations. It progresses from elementary materials to methods used in the design of NACA low-drag airfoils, and it presents techniques for using wing-section data to predict wing characteristics. Requires differential and integral calculus and elementary mechanics. 1949 edition.
ArbetstitelTheory of wing sections
Standardpris349.00
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Orginaltitel
Åldersgrupp
BandtypHäftad
Recensionsutdrag
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Sidor703
Publiceringsdatum1959-06-01 00:00:00
FörfattareA.E.Von Doenhoff
Kort BeskrivningA reference for engineers and students, this volume devotes more than 300 pages to theoretical and experimental considerations. It progresses from elementary materials to methods used in the design of NACA low-drag airfoils, and it presents techniques for using wing-section data to predict wing characteristics. Requires differential and integral calculus and elementary mechanics. 1949 edition.
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