Author: William A. Jr NewsonPublisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane: Wind-tunnel Investigation of High-angle-of-attack Aerodynamic Characteristics
Author: William A. Jr NewsonPublisher:
ISBN:
Category :
Languages : en
Pages : 112
Book Description
Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane
Author: William A. NewsomPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 112
Book Description
NASA Technical Paper
Author: Effects of Wing-leading-edge Modifications on a Full-scale, Low-wing General Aviation Airplane
Author: William A. NewsomPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104
Book Description
NASA Technical Memorandum
Author: Scientific and Technical Aerospace Reports
Author: Simulator Study of the Stall Departure Characteristics of a Light General Aviation Airplane with and Without a Wing-leading-edge Modification
Author: Donald R. RileyPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 92
Book Description
Spin Recovery Training
Author: United States. Congress. House. Committee on Science and Technology. Subcommittee on Investigations and OversightPublisher:
ISBN:
Category : Flight training
Languages : en
Pages : 246
Book Description
Computational Fluid Dynamics
Author: John WendtPublisher: Springer Science & Business Media
ISBN: 3540850554
Category : Technology & Engineering
Languages : en
Pages : 333
Book Description
Computational Fluid Dynamics: An Introduction grew out of a von Karman Institute (VKI) Lecture Series by the same title ?rst presented in 1985 and repeated with modi?cations every year since that time. The objective, then and now, was to present the subject of computational ?uid dynamics (CFD) to an audience unfamiliar with all but the most basic numerical techniques and to do so in such a way that the practical application of CFD would become clear to everyone. A second edition appeared in 1995 with updates to all the chapters and when that printing came to an end, the publisher requested that the editor and authors consider the preparation of a third edition. Happily, the authors received the request with enthusiasm. The third edition has the goal of presenting additional updates and clari?cations while preserving the introductory nature of the material. The book is divided into three parts. John Anderson lays out the subject in Part I by ?rst describing the governing equations of ?uid dynamics, concentrating on their mathematical properties which contain the keys to the choice of the numerical approach. Methods of discretizing the equations are discussed and transformation techniques and grids are presented. Two examples of numerical methods close out this part of the book: source and vortex panel methods and the explicit method. Part II is devoted to four self-contained chapters on more advanced material. Roger Grundmann treats the boundary layer equations and methods of solution.
Research Abstracts
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description