Author: United States. National Aeronautics and Space Administration. Ad Hoc Committee on Subsonic and Supersonic AeronauticsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Some Fluid Mechanical Problems Related to Subsonic and Supersonic Aircraft
Author: United States. National Aeronautics and Space Administration. Ad Hoc Committee on Subsonic and Supersonic AeronauticsPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
Book Description
Monthly Catalog of United States Government Publications
Author: NASA SP.
Author: National Union Catalog
Author: Publisher:
ISBN:
Category : Union catalogs
Languages : en
Pages : 808
Book Description
Includes entries for maps and atlases.
The National Union Catalogs, 1963-
Author: The National union catalog, 1968-1972
Author: American Book Publishing Record Cumulative, 1950-1977
Author: R.R. Bowker Company. Department of BibliographyPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1434
Book Description
American Book Publishing Record Cumulative 1950-1977
Author: R.R. Bowker CompanyPublisher: R. R. Bowker
ISBN:
Category : Bibliography, National
Languages : en
Pages : 1442
Book Description
Library of Congress Catalogs
Author: Library of CongressAircraft Conceptual Design Synthesis
Author: Denis HowePublisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 488
Book Description
Aircraft Conceptual Design Synthesis means design by fitness-for-purpose. Design engineers can jump off from the point of given parameters and requirements – required performance, payloads and other factors. This is the first book for the aeronautical designer devoted to guiding the reader through this highly effective conceptual design synthesis process. This forms the procedure for the initial stage of the aircraft design process – the interpretation of a requirement into the preliminary layout. A logical design sequence is developed utilizing original modules to represent propulsion, lift, drag, mass, and performance. Aircraft Conceptual Design Synthesis includes a disk of spreadsheets that provides core data. Unlike existing approaches, the design synthesis method can be applied to novel aircraft concepts. CONTENTS INCLUDE The design process Aircraft configuration Flight regime and powerplant considerations Fuselage layout Configuration of the wing Basic lift, drag and mass representations Performance estimation Parametric analysis and optimisation Analysis of concept design “This is an important landmark book and in my view will become a standard by which others will be compared” – Dr E C P Ransom, Kingston University, UK