Scientific and Technical Aerospace Reports
Author :
Publisher :
Page : 1158 pages
File Size : 13,10 MB
Release : 1965
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1158 pages
File Size : 13,10 MB
Release : 1965
Category : Aeronautics
ISBN :
Author : Robert C. Nelson
Publisher :
Page : 464 pages
File Size : 33,29 MB
Release : 1998
Category : History
ISBN :
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 49,39 MB
Release : 2003
Category : Aerodynamics
ISBN : 9781600860782
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author : Snorri Gudmundsson
Publisher : Butterworth-Heinemann
Page : 1058 pages
File Size : 32,39 MB
Release : 2013-09-03
Category : Technology & Engineering
ISBN : 0123973295
Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design. - Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need - Numerical examples involve actual aircraft specs - Contains high-interest topics not found in other texts, including sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design - Provides a unique safety-oriented design checklist based on industry experience - Discusses advantages and disadvantages of using computational tools during the design process - Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution - Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs - Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only)
Author : Gerald V. Foster
Publisher :
Page : 32 pages
File Size : 35,81 MB
Release : 1960
Category : Aerodynamics
ISBN :
Author : Francis J. Capone
Publisher :
Page : 308 pages
File Size : 30,82 MB
Release : 1980
Category :
ISBN :
Author : Daniel P. Raymer
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 0 pages
File Size : 47,74 MB
Release : 2006
Category : Airplanes
ISBN : 9781563478291
Winner of the Summerfield Book Award Winner of the Aviation-Space Writers Association Award of Excellence. --Over 30,000 copies sold, consistently the top-selling AIAA textbook title This highly regarded textbook presents the entire process of aircraft conceptual designfrom requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studiesin the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 800 pages of design methods, illustrations, tips, explanations, and equations, and extensive appendices with key data essential to design. It is the required design text at numerous universities around the world, and is a favorite of practicing design engineers.
Author : Donald L. Loving
Publisher :
Page : 20 pages
File Size : 33,46 MB
Release : 1966
Category : Aerodynamic load
ISBN :
Author :
Publisher :
Page : 236 pages
File Size : 22,54 MB
Release : 1979
Category :
ISBN :
Author : Curtis Peebles
Publisher :
Page : 334 pages
File Size : 33,77 MB
Release : 2014-12-10
Category : Research aircraft
ISBN : 9781626830219
With the development of supersonic aircraft, the X-plane era ushered in a new and challenging phase of flight. Researchers found that much of the knowledge accumulated from the previous, subsonic flight era did not apply to the emerging supersonic aircraft. These turbojet-powered planes also outpaced the usefulness of the wind tunnel, previously an indispensible tool of aeronautic research.This book explores the development of the X-series research aircraft, the planes that helped bridge the gap between subsonic flight and hypersonic flight.