Author: K. StewartsonPublisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
On Wing-body Interference in Supersonic Flow
Author: K. StewartsonThe Wing-body Interference Problem for Linearized Supersonic Flow
Author: Michael Chen-Chiang FongPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68
Book Description
Potential Flow Approach for Wing-body Interference for Missiles in Supersonic Flow
Author: Milind V. TalpallikarReverse Flow and Supersonic Interference
Author: Brown University. Division of EngineeringPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 106
Book Description
Numerical Solutions to Wing-body Interference of Missiles in Supersonic Flow
Author: Milind TalpallikarAn Integrated Approach to the Analysis and Design of Wings and Wing-body Combinations in Supersonic Flow
Author: Ralph L. CarmichaelPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
An Extension of the Linearised Theory of Supersonic Flow Past Quasi-cylindrical Bodies, with Applications to Wing-body Interference
Author: R. C. LockAn Investigation of the Lift and Wing-body Interference of Rectangular Finned Missiles in Supersonic Flow
Author: Edward Frederick SpraitzPublisher:
ISBN:
Category :
Languages : en
Pages : 38
Book Description
Analysis of the Effect of Wing-wing Interference on the Rolling Characteristics of Cruciform Rectangular Wing-body Combinations in Steady Supersonic Flow
Author: G. V. BullWing Theory in Supersonic Flow
Author: Elie CarafoliPublisher: Elsevier
ISBN: 1483160270
Category : Technology & Engineering
Languages : en
Pages : 611
Book Description
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 characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.