Airplane Aerodynamics and Performance
Author : Jan Roskam
Publisher : DARcorporation
Page : 748 pages
File Size : 12,60 MB
Release : 1997
Category : Science
ISBN : 9781884885440
Author : Jan Roskam
Publisher : DARcorporation
Page : 748 pages
File Size : 12,60 MB
Release : 1997
Category : Science
ISBN : 9781884885440
Author : John David Anderson
Publisher : McGraw-Hill Science, Engineering & Mathematics
Page : 602 pages
File Size : 41,85 MB
Release : 1999
Category : Technology & Engineering
ISBN :
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 : Mario Asselin
Publisher : AIAA
Page : 366 pages
File Size : 17,73 MB
Release : 1997
Category : Airplanes
ISBN : 9781600860249
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 39,36 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 : Maido Saarlas
Publisher : John Wiley & Sons
Page : 298 pages
File Size : 40,19 MB
Release : 2006-12-05
Category : Technology & Engineering
ISBN : 0470044160
Aircraft PERFORMANCE STRAIGHTFORWARD METHODS TO DESIGN AND OPERATE AIRCRAFT TO MEET PERFORMANCE SPECIFICATIONS Aircraft Performance sets forth a group of tested and proven methods needed to determine the performance of an aircraft. The central theme of this book is the energy method, which enhances understanding of the standard methods and provides accessibility to advanced topics. As a result, readers gain a thorough understanding of the performance issues involved in operating an aircraft in an efficient and economic manner. While covering all the standard topics—level and climbing flight, range and endurance, take-off and landing, and maneuvering flight—the book focuses on the energy methods applied to path performance analysis. Throughout the text, numerous examples from both the commercial and military sectors show readers how the concepts and calculations are applied to real-life situations. Problems, ranging from basic to complex, test the readers’ understanding and provide an opportunity for essential practice. To help focus the readers’ attention on core issues, this text assumes that aerodynamics and propulsion are known inputs. Special appendices are provided to present some aerodynamic and propulsive equations and data. In general, topics are separated into horizontal and vertical plane approaches. Following an introduction and overview, basic energy concepts are employed to obtain a fundamental performance equation. This text, with its extensive use of examples and problem sets, is ideal for upper- level undergraduate and graduate students in engineering. It also serves as a reference for design engineers in both military and industrial sectors who want a set of clear and reliable methods to calculate aircraft performance.
Author : Bandu N. Pamadi
Publisher : AIAA
Page : 810 pages
File Size : 10,61 MB
Release : 2004
Category : Aerodynamics
ISBN : 9781600860997
Author : W. Austyn Mair
Publisher : Cambridge University Press
Page : 334 pages
File Size : 33,32 MB
Release : 1996-03-14
Category : Science
ISBN : 9780521568364
Describes the principles and equations required for evaluating the performance of an aircraft.
Author : Antonio Filippone
Publisher : Cambridge University Press
Page : 665 pages
File Size : 29,26 MB
Release : 2012-12-17
Category : Technology & Engineering
ISBN : 113978966X
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 : Charles E. Dole
Publisher : John Wiley & Sons
Page : 384 pages
File Size : 43,49 MB
Release : 2016-11-21
Category : Technology & Engineering
ISBN : 1119233402
The pilot's guide to aeronautics and the complex forces of flight Flight Theory and Aerodynamics is the essential pilot's guide to the physics of flight, designed specifically for those with limited engineering experience. From the basics of forces and vectors to craft-specific applications, this book explains the mechanics behind the pilot's everyday operational tasks. The discussion focuses on the concepts themselves, using only enough algebra and trigonometry to illustrate key concepts without getting bogged down in complex calculations, and then delves into the specific applications for jets, propeller crafts, and helicopters. This updated third edition includes new chapters on Flight Environment, Aircraft Structures, and UAS-UAV Flight Theory, with updated craft examples, component photos, and diagrams throughout. FAA-aligned questions and regulatory references help reinforce important concepts, and additional worked problems provide clarification on complex topics. Modern flight control systems are becoming more complex and more varied between aircrafts, making it essential for pilots to understand the aerodynamics of flight before they ever step into a cockpit. This book provides clear explanations and flight-specific examples of the physics every pilot must know. Review the basic physics of flight Understand the applications to specific types of aircraft Learn why takeoff and landing entail special considerations Examine the force concepts behind stability and control As a pilot, your job is to balance the effects of design, weight, load factors, and gravity during flight maneuvers, stalls, high- or low-speed flight, takeoff and landing, and more. As aircraft grow more complex and the controls become more involved, an intuitive grasp of the physics of flight is your most valuable tool for operational safety. Flight Theory and Aerodynamics is the essential resource every pilot needs for a clear understanding of the forces they control.
Author : Peter J. Swatton
Publisher : John Wiley & Sons
Page : 384 pages
File Size : 41,63 MB
Release : 2008-04-30
Category : Technology & Engineering
ISBN : 0470693053
The new European Joint Aviation Requirements (JARs) lay down rules governing the minimum levels of performance which must be attained by every type of public transport aeroplane. These rules cover matters such as weight, altitude and temperature, take-off and landing distance, cruise flight level and speed, and descent angle and rate. The subject of aircraft performance forms an important part of all JAR Flight Crew Licensing examinations for commercial and airline transport pilot licences, and this book provides a clear but authoritative text on a difficult topic. It will also be of interest to commercial pilots needing to upgrade their annual ground test to JAR standards, and to flight planners, operations controllers and airport operators.