Flight Performance of Fixed and Rotary Wing Aircraft

Flight Performance of Fixed and Rotary Wing Aircraft
Author: Antonio Filippone
Publisher: Elsevier
Total Pages: 594
Release: 2006-05-10
Genre: Technology & Engineering
ISBN: 0080461034

Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more.This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft. - Unique coverage of fixed and rotary wing aircraft in a unified manner, including optimisation, emissions control and regulation. - Ideal for students, aeronautical engineering capstone projects, and for widespread professional reference in the aerospace industry. - Comprehensive coverage of computer-based solution of aerospace engineering problems; the critical analysis of performance data; and case studies from real world engineering experience. - Supported by end of chapter exercises

The Future of Aerospace

The Future of Aerospace
Author: National Academy of Engineering
Publisher: National Academies Press
Total Pages: 88
Release: 1993-02-01
Genre: Technology & Engineering
ISBN: 0309048818

Few technological advances have affected the lives and dreams of individuals and the operations of companies and governments as much as the continuing development of flight. From space exploration to package transport, from military transport to passenger helicopter use, from passenger jumbo jets to tilt-rotor commuter planes, the future of flying is still rapidly developing. The essays in this volume survey the state of progress along several fronts of this constantly evolving frontier. Five eminent authorities assess prospects for the future of rotary-wing aircraft, large passenger aircraft, commercial aviation, manned spaceflight, and defense aerospace in the post-Cold War era.

Rotary-Wing Aerodynamics

Rotary-Wing Aerodynamics
Author: W. Z. Stepniewski
Publisher: Courier Corporation
Total Pages: 640
Release: 2013-04-22
Genre: Technology & Engineering
ISBN: 0486318516

DIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div

Rotorcraft Aeromechanics

Rotorcraft Aeromechanics
Author: Wayne Johnson
Publisher: Cambridge University Press
Total Pages: 949
Release: 2013-04-29
Genre: Technology & Engineering
ISBN: 1107355281

A rotorcraft is a class of aircraft that uses large-diameter rotating wings to accomplish efficient vertical take-off and landing. The class encompasses helicopters of numerous configurations (single main rotor and tail rotor, tandem rotors, coaxial rotors), tilting proprotor aircraft, compound helicopters, and many other innovative configuration concepts. Aeromechanics covers much of what the rotorcraft engineer needs: performance, loads, vibration, stability, flight dynamics, and noise. These topics include many of the key performance attributes and the often-encountered problems in rotorcraft designs. This comprehensive book presents, in depth, what engineers need to know about modelling rotorcraft aeromechanics. The focus is on analysis, and calculated results are presented to illustrate analysis characteristics and rotor behaviour. The first third of the book is an introduction to rotorcraft aerodynamics, blade motion, and performance. The remainder of the book covers advanced topics in rotary wing aerodynamics and dynamics.

Rotary Wing Flight

Rotary Wing Flight
Author: U S Army
Publisher: Aviation Supplies & Academics
Total Pages: 122
Release: 2001
Genre: History
ISBN: 9781560271185

Helicopter aerodynamics, common flight techniques, normal field operations, and precautionary measures and critical conditions are discussed. This is U.S. Army handbook FM 1-51.

Fixed Wing Flight

Fixed Wing Flight
Author: United States. Department of the Army
Publisher:
Total Pages: 102
Release: 1968
Genre: Airplanes
ISBN:

Rotary Wing Flight

Rotary Wing Flight
Author: United States. Department of the Army
Publisher:
Total Pages: 172
Release: 1974
Genre: Helicopters
ISBN:

Helicopter Theory

Helicopter Theory
Author: Wayne Johnson
Publisher: Courier Corporation
Total Pages: 1126
Release: 1994-01-01
Genre: Technology & Engineering
ISBN: 9780486682303

The history of the helicopter may be traced back to the Chinese flying top (c. 400 BC) and to the work of Leonardo da Vinci, who sketched designs for a vertical flight machine utilizing a screw-type propeller. In the late 19th-century, Thomas Edison experimented with helicopter models, realizing that no such machine would be able to fly until the development of a sufficiently lightweight engine. When the internal combustion gasoline engine came on the scene around 1900, the stage was set for the real development of helicopter technology. While this text provides a concise history of helicopter development, its true purpose is to provide the engineering analysis required to design a highly successful rotorcraft. Toward that end the book offers thorough, comprehensive coverage of the theory of helicopter flight: the elements of vertical flight, forward flight, performance, design, mathematics of rotating systems, rotary wing dynamics and aerodynamics, aeroelasticity, stability and control, stall, noise and more. Wayne Johnson has worked for the U.S. Army and NASA at the Ames Research Center in California. Through his company Johnson Aeronautics, he is engaged in the development of software that is used throughout the world for the analysis of rotorcraft. In this book, Dr. Johnson has compiled a monumental resource that is essential reading for any student or aeronautical engineer interested in the design and development of vertical-flight aircraft.

Flight Testing of Fixed Wing Aircraft

Flight Testing of Fixed Wing Aircraft
Author: Ralph D. Kimberlin
Publisher: AIAA
Total Pages: 464
Release: 2003
Genre: Airplanes
ISBN: 9781600860560

Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.