Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces
Title | Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces PDF eBook |
Author | Jacob H. Lichtenstein |
Publisher | |
Pages | 40 |
Release | 1951 |
Genre | Airplanes |
ISBN |
Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.
Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces
Title | Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces PDF eBook |
Author | Arthur Earl Bryson |
Publisher | |
Pages | 340 |
Release | 1952 |
Genre | Aeronautics |
ISBN |
Index of NACA Technical Publications
Title | Index of NACA Technical Publications PDF eBook |
Author | United States. National Advisory Committee for Aeronautics |
Publisher | |
Pages | 258 |
Release | 1953 |
Genre | Aeronautics |
ISBN |
NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls
Title | NASA's Contributions to Aeronautics: Aerodynamics, structures, propulsion, controls PDF eBook |
Author | |
Publisher | |
Pages | 980 |
Release | 2010 |
Genre | Aeronautics |
ISBN |
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.
NASA's Contributions to Aeronautics
Title | NASA's Contributions to Aeronautics PDF eBook |
Author | |
Publisher | |
Pages | 980 |
Release | 2010 |
Genre | Aeronautics |
ISBN |
Monthly Catalog of United States Government Publications
Title | Monthly Catalog of United States Government Publications PDF eBook |
Author | United States. Superintendent of Documents |
Publisher | |
Pages | 1714 |
Release | 1959 |
Genre | Government publications |
ISBN |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Stability and Control of Airplanes and Helicopters
Title | Stability and Control of Airplanes and Helicopters PDF eBook |
Author | Edward Seckel |
Publisher | Academic Press |
Pages | 523 |
Release | 2014-05-10 |
Genre | Technology & Engineering |
ISBN | 148322015X |
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.