Author: Edward Charles PolhamusPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 86
Book Description
The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Author: Edward C. PolhamusPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
Book Description
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Author: Edward Charles PolhamusPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 86
Book Description
The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Author: Edward C. PolhamusPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 81
Book Description
NASA Technical Note
Author: Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: Index of N A S A Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 498
Book Description
Index of NASA Technical Publications
Author: Index to NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 300
Book Description
Stability and Control of Airplanes and Helicopters
Author: Edward SeckelPublisher: Academic Press
ISBN: 148322015X
Category : Technology & Engineering
Languages : en
Pages : 523
Book Description
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.