Wing theory in supersonic flow /

Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more co...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores principales: Carafoli, Elie, Mateescu, Dan (Autor), N�astase, Adriana (Autor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Oxford ; New York : Pergamon Press, [1969]
Edición:[1st ed.].
Colección:International series of monographs in aeronautics and astronautics. Aerodynamics ; v. 7.
Temas:
Aerodynamics, Supersonic.
Airplanes > Wings.
A�erodynamique supersonique.
Avions > Ailes.
TECHNOLOGY & ENGINEERING > Engineering (General)
Aerodynamics, Supersonic
Airplanes > Wings
Bemessungsgrundlage
Berechnung
Deltafl�ugel
�Uberschallstr�omung
Aeroplanes > Wings
Acceso en línea:Texto completo
Descripción
Sumario:Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the.
Descripción Física:1 online resource (xiii, 594 pages)
Bibliografía:Includes bibliographical references (pages 565-588).
ISBN:9781483160276
1483160270

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