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Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Wing On And Wing Off Longitudinal Characteristics Of An Airplane Configuration Having A Thin Unswept Wing Of Aspect Ratio 3 As Obtained From Rocket Propelled Models At Mach Numbers From 0 8 To 1 4 book. This book definitely worth reading, it is an incredibly well-written.
Author : Anonim
Publisher : Unknown
Page : 388 pages
File Size : 44,6 Mb
Release : 1957
Category : Aeronautics
ISBN : UVA:X004173287
Author : Clarence L. Gillis,A. James Vitale
Publisher : Unknown
Page : 46 pages
File Size : 48,7 Mb
Release : 1959
Category : Mach number
ISBN : UIUC:30112106741579
Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 388 pages
File Size : 41,5 Mb
Release : 1959
Category : Aeronautics
ISBN : UCBK:C029901327
Author : Robert C. Nelson
Publisher : WCB/McGraw-Hill
Page : 441 pages
File Size : 49,8 Mb
Release : 1998
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
ISBN : 0071158383
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author : Bruce Larrimer
Publisher : Unknown
Page : 128 pages
File Size : 45,8 Mb
Release : 2020-06-15
Category : Electronic
ISBN : 1626830592
Author : Antonio Filippone
Publisher : Cambridge University Press
Page : 665 pages
File Size : 50,8 Mb
Release : 2012-12-17
Category : Technology & Engineering
ISBN : 9781139789660
This book discusses aircraft flight performance, focusing on commercial aircraft but also considering examples of high-performance military aircraft. The framework is a multidisciplinary engineering analysis, fully supported by flight simulation, with software validation at several levels. The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of environmental performance. A unique feature of this book is the discussion and analysis of the environmental performance of the aircraft, focusing on topics such as aircraft noise and carbon dioxide emissions.
Author : R. Dale Reed,Darlene Lister
Publisher : University Press of Kentucky
Page : 404 pages
File Size : 52,5 Mb
Release : 2021-10-21
Category : Technology & Engineering
ISBN : 9780813185637
Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
Author : John David Anderson
Publisher : McGraw-Hill Science, Engineering & Mathematics
Page : 602 pages
File Size : 52,7 Mb
Release : 1999
Category : Technology & Engineering
ISBN : MINN:31951D01655193L
Balancing technical material with important historical aspects of the invention and design of aeroplanes, this book develops aircraft performance techniques from first principles and applies them to real aeroplanes.
Author : Donald L. Loving
Publisher : Unknown
Page : 20 pages
File Size : 46,8 Mb
Release : 1966
Category : Aerodynamic load
ISBN : UIUC:30112106686881
Author : Holt Ashley,Mårten Landahl,Marten T. Landahl
Publisher : Courier Corporation
Page : 306 pages
File Size : 40,6 Mb
Release : 1965-01-01
Category : Technology & Engineering
ISBN : 9780486648996
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
Author : Joseph R. Chambers
Publisher : Unknown
Page : 406 pages
File Size : 48,5 Mb
Release : 2005
Category : Aeronautics
ISBN : IND:30000109243109
Author : Peter W. Merlin
Publisher : Unknown
Page : 293 pages
File Size : 48,9 Mb
Release : 2015
Category : U-2 (Reconnaissance aircraft)
ISBN : 1626830258
Designed as a stopgap measure to provide overhead reconnaissance capability during the early years of the Cold War, the versatile U-2 has since evolved to meet changing requirements well into the 21st century. Though many authors have documented the airplane's operational history, few have made more than a cursory examination of its technical aspects or its role as a NASA research platform. This volume includes an overview of the origin and development of the Lockheed U-2 family of aircraft with early National Advisory Committee for Aeronautics (NACA) and National Aeronautics and Space Administration (NASA) involvement, construction and materials challenges faced by designers and builders, releasable performance characteristics and capabilities, use of U-2 and ER-2 airplanes as research platforms, and technical and programmatic lessons learned.
Author : John H. Blakelock
Publisher : John Wiley & Sons
Page : 668 pages
File Size : 54,8 Mb
Release : 1991-09-03
Category : Technology & Engineering
ISBN : 0471506516
This Second Edition continues the fine tradition of its predecessor by exploring the various automatic control systems in aircraft and on board missiles. Considerably expanded and updated, it now includes new or additional material on: the effectiveness of beta-beta feedback as a method of obtaining coordination during turns using the F-15 as the aircraft model; the root locus analysis of a generic acceleration autopilot used in many air-to-air and surface-to-air guided missiles; the guidance systems of the AIM-9L Sidewinder as well as bank-to-turn missiles; various types of guidance, including proportional navigation and line-of-sight and lead-angle command guidance; the coupling of the output of a director fire control system into the autopilot; the analysis of multivariable control systems; and methods for modeling the human pilot, plus the integration of the human pilot into an aircraft flight control system. Also features many new additions to the appendices.
Author : Cliff Matthews
Publisher : Elsevier
Page : 288 pages
File Size : 51,6 Mb
Release : 2001-10-17
Category : Technology & Engineering
ISBN : 9780080488288
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
Author : Lloyd R. Jenkinson,Jim Marchman
Publisher : Elsevier
Page : 400 pages
File Size : 45,7 Mb
Release : 2003-04-28
Category : Business & Economics
ISBN : 9780080498959
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
