An Investigation At Subsonic Speeds Of The Longitudinal Aerodynamic Characteristics At Angles Of Attach From 4 To 100 Of Delta Wing Reentry Configurations Having Vertically Displaced And Cambered Wing Tip Panels
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Author | : Bernard Spencer |
Publisher | : |
Total Pages | : 40 |
Release | : 1961 |
Genre | : Aerodynamics |
ISBN | : |
Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.
Author | : |
Publisher | : |
Total Pages | : 1074 |
Release | : 1963 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : Bernard Spencer |
Publisher | : |
Total Pages | : 34 |
Release | : 1959 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Frank Hitchens |
Publisher | : Andrews UK Limited |
Total Pages | : 877 |
Release | : 2015-11-25 |
Genre | : Science |
ISBN | : 1785383256 |
The Encyclopedia of Aerodynamics was written for pilots at all levels from private pilot to airline pilot, military pilots and students of aerodynamics as a complete reference manual to aerodynamic terminology. General aerodynamic text books for pilots are relatively limited in their scope while aerodynamic text books for engineering students involve complex calculus. The references in this book, The Encyclopedia of Aerodynamics, are clearly described and only basic algebra is used in a few references but is completely devoid of any calculus - an advantage to many readers. Over 1400 references are included with alternative terms used where appropriate and cross-referenced throughout. The text is illustrated with 178 photographs and 96 diagrams. The Encyclopedia of Aerodynamics is an ideal aerodynamic reference manual for any pilot's bookshelf.
Author | : Donald L. Loving |
Publisher | : |
Total Pages | : 20 |
Release | : 1966 |
Genre | : Aerodynamic load |
ISBN | : |
Author | : R. Dale Reed, Darlene Lister |
Publisher | : University Press of Kentucky |
Total Pages | : 260 |
Release | : |
Genre | : Technology & Engineering |
ISBN | : 9780813132228 |
"Much has been written about the famous conflicts and battlegrounds of the East during the American Revolution. Perhaps less familiar, but equally important and exciting, was the war on the western frontier, where Ohio Valley settlers fought for the land they had claimed -- and for their very lives. George Rogers Clark stepped forward to organize the local militias into a united front that would defend the western frontier from Indian attacks. Clark was one of the few people who saw the importance of the West in the war effort as a whole, and he persuaded Virginia's government to lend support to his efforts. As a result Clark was able to cross the Ohio, saving that part of the frontier from further raids. Lowell Harrison captures the excitement of this vital part of American history while giving a complete view of George Rogers Clark's significant achievements. Lowell H. Harrison, is a professor emeritus of history at Western Kentucky University and is the author or co-author of numerous books, including Lincoln of Kentucky, A New History of Kentucky, and Kentucky's Governors."
Author | : Bernard Etkin |
Publisher | : John Wiley & Sons |
Total Pages | : 392 |
Release | : 1982 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : Charles F. Reid |
Publisher | : |
Total Pages | : 36 |
Release | : 1961 |
Genre | : Oscillations |
ISBN | : |
Author | : Michael V. Cook |
Publisher | : Butterworth-Heinemann |
Total Pages | : 608 |
Release | : 2012-10-03 |
Genre | : Technology & Engineering |
ISBN | : 008098276X |
The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. - Additional examples to illustrate the application of computational procedures using tools such as MATLAB®, MathCad® and Program CC® - Improved compatibility with, and more expansive coverage of the North American notational style - Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence - An additional coursework study on flight control design for an unmanned air vehicle (UAV)
Author | : A. G. Panaras |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 0 |
Release | : 2012 |
Genre | : Aerodynamics |
ISBN | : 9781600869167 |
In "Aerodynamic Principles of Flight Vehicles" Argyris Panaras examines the fundamentals of vortices and shock waves, aerodynamic estimation of lift and drag, airfoil theory, boundary layer control, and high-speed, high-temperature flow. Individual chapters address vortices in aerodynamics, transonic and supersonic flows, transonic/supersonic aircraft configurations, and high-supersonic/hypersonic flows, beginning with definitions and historical data, and then describing present-day status and current research challenges. Emphasis is given to flow control, to the evolution of flight vehicle shapes as flight speed has increased, and to discoveries that enabled breakthrough developments in flight. The book: examines why various equations and technologies were developed, explains major contributors in areas such as vortices and aircraft wakes, drag buildup, sonic boom, and shock wave-boundary layer interactions, among others, and helps readers apply concepts from the material to their own projects. Archival and encyclopedic, "Aerodynamic Principles of Flight Vehicles" is a superb reference for aeronautical students and professionals alike. Although most beneficial to readers with a working knowledge of aerodynamics, it is accessible to anyone with an introductory understanding of the field.