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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...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford ; New York :
Pergamon Press,
[1969]
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| Edición: | [1st ed.]. |
| Colección: | International series of monographs in aeronautics and astronautics. Aerodynamics ;
v. 7. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Wing Theory in Supersonic Flow; Copyright Page; Table of Contents; PREFACE; ACKNOWLEDGEMENTS; CHAPTER I. RECAPITULATIVE SURVEY OF THE EQUATIONS OF MOTIONOF PERFECT FLUIDS IN SUPERSONIC FLOW; I. 1. General Equations; I. 2. Propagation of Small Disturbances; I. 3. Velocity Potential Equation; I. 4. Pressure Coefficient under the Assumption of Small Disturbances; I. 5. Theory of Wings of Infinite Aspect Ratio in Supersonic Flow underthe Assumption of Small Disturbances.
- I. 6. Theory of Axially-symmetric Bodies under the Assumption of SmallDisturbances (Application to the Circular Cone)I. 7. Conical Motions in Supersonic Flow; I. 8. High-order Conical Flows; CHAPTER II. UNIFIED THEORY OF ANGULAR WINGS BASED ON HIGH-ORDERCONICAL FLOW DETERMINATION OF THE AXIAL DISTURBANCE VELOCITY(u) AND OF THE DOWNWASH (w) IN THE DIRECT, INDIRECT ANDMIXED PROBLEMS; II. 1. General Considerations; CHAPTERIII. THE CALCULATION OF THE OVERALL FORCES AND MOMENTS ONWINGS WITH TRAILING EDGES OF ARBITRARY PLANFORM SHAPE.
- II. 2. Behaviour of the Axial Disturbance Velocity u in the Neighbourhoodof the Subsonic Leading Edges or the Subsonic Ridges on the ThinWing (Direct Problem)II. 3. Contribution of the Subsonic Leading Edges of Thin Wings and of the Separation Ridges to the Construction of the Velocity u (DirectProblem); II. 4. Examples of Application to Ordinary Wings in the Direct Problem; II. 5. Determination of Constants; II. 6. Examples of the Determination of Constants.
- II. 7. Contribution of the Ridges and the Leading Edge to the Calculation ofthe Downwash w, when the Pressures are given on the Wing(Indirect Problem)II. 8. Some Considerations on the Indirect Problem; II. 9. Wing whose Incidence Variation and Pressure Distribution are givenAlternatively on Separate Portions (Mixed Problem); III. 1. Preliminary Considerations; III. 2. Calculation of Forces; III. 3. Calculation of Moments; III. 4. Some Special Applications of the Formulae for Calculating the Forcesand Moments.
- III. 5. Calculation of the Suction Force induced by the Subsonic LeadingEdges of a Thin WingCHAPTERIV. STUDY OF ORDINARY DELTA WINGS; IV. 1. Introductory Considerations on the Delta Wing; IV. 2. Thin Delta Wing with Subsonic Leading Edges having SymmetricalIncidences; IV. 3. Thin Delta Wing with Subsonic Edges having Antisymmetrical Incidences; IV. 4. Thin Delta Wing with Supersonic Edges and Symmetry of Incidence; IV. 5. Wing of Symmetrical Thickness; IV. 6. Thin Delta Wing with Supersonic Edges and Antisymmetry of Incidence; IV. 7. Delta Wing with Sonic Leading Edges.