Author: A. J. EggersPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 284
Book Description
The Effect of Blade-section Thickness Ratios on the Aerodynamic Characteristics of Related Full-scale Propellers at Mach Numbers Up to 0.65
Author: A. J. EggersPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 284
Book Description
Government reports annual index
Author: Theory of Wing Sections
Author: Ira H. AbbottPublisher: Courier Corporation
ISBN: 0486134997
Category : Technology & Engineering
Languages : en
Pages : 708
Book Description
Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
Aerofoil Sections
Author: Friedrich Wilhelm RiegelsPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 281
Book Description
Aircraft Design Projects
Author: Lloyd R. JenkinsonPublisher: Elsevier
ISBN: 0080498957
Category : Technology & Engineering
Languages : en
Pages : 393
Book Description
Written with students of aerospace or aeronautical engineering firmly in mind, this is a practical and wide-ranging book that draws together the various theoretical elements of aircraft design - structures, aerodynamics, propulsion, control and others - and guides the reader in applying them in practice. Based on a range of detailed real-life aircraft design projects, including military training, commercial and concept aircraft, the experienced UK and US based authors present engineering students with an essential toolkit and reference to support their own project work.All aircraft projects are unique and it is impossible to provide a template for the work involved in the design process. However, with the knowledge of the steps in the initial design process and of previous experience from similar projects, students will be freer to concentrate on the innovative and analytical aspects of their course project. The authors bring a unique combination of perspectives and experience to this text. It reflects both British and American academic practices in teaching aircraft design. Lloyd Jenkinson has taught aircraft design at both Loughborough and Southampton universities in the UK and Jim Marchman has taught both aircraft and spacecraft design at Virginia Tech in the US.* Demonstrates how basic aircraft design processes can be successfully applied in reality* Case studies allow both student and instructor to examine particular design challenges * Covers commercial and successful student design projects, and includes over 200 high quality illustrations
Aeronautical Engineer's Data Book
Author: Cliff MatthewsPublisher: Elsevier
ISBN: 0080488285
Category : Technology & Engineering
Languages : en
Pages : 282
Book Description
Aeronautical Engineer's Data Bookis an essential handy guide containing useful up to date information regularly needed by the student or practising engineer. Covering all aspects of aircraft, both fixed wing and rotary craft, this pocket book provides quick access to useful aeronautical engineering data and sources of information for further in-depth information. - Quick reference to essential data - Most up to date information available
Gas Turbine Performance
Author: Philip P. WalshPublisher: John Wiley & Sons
ISBN: 140515103X
Category : Technology & Engineering
Languages : en
Pages : 664
Book Description
A significant addition to the literature on gas turbine technology, the second edition of Gas Turbine Performance is a lengthy text covering product advances and technological developments. Including extensive figures, charts, tables and formulae, this book will interest everyone concerned with gas turbine technology, whether they are designers, marketing staff or users.
Scientific and Technical Aerospace Reports
Author: Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils from Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel
Author: Albert E. Von DoenhoffPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 24
Book Description
Summary: Two low-drag airfoils, the NACA 747A315 and the NACA 747A415, designed to have reduced pitching moments about the quarter-chord point and moderately high values of the design lift coefficient have been tested in the NACA two-dimensional low-turbulence pressure tunnel. Section lift, drag, and pitching-moment coefficients are presented for Reynolds numbers of 3 x 106, 6 x 106, and 9 x 106, together with section lift and section drag data for a Reynolds number of 6 x 106 for the same airfoils with roughened leading edges.
Rotodynamic Pumps (Centrifugal and Axial)
Author: K. M. SrinivasanPublisher: New Age International
ISBN: 8122422780
Category : Axial flow pumps
Languages : en
Pages : 15
Book Description