Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack PDF Download
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Author: Russell W. McDearmon Publisher: ISBN: Category : Airplanes Languages : en Pages : 42
Book Description
Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.
Author: Russell W. McDearmon Publisher: ISBN: Category : Airplanes Languages : en Pages : 42
Book Description
Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.
Author: Macon C. Ellis Publisher: ISBN: Category : Aerodynamic, Supersonic Languages : en Pages : 44
Book Description
Results from a supersonic wind-tunnel investigation of a series of thin triangular and sweptback wings are presented. The triangular wing series consisted of eight triangular wings of vertex angles such that a range of leading-edge postions both inside and outside the Mach cone at the test Mach numbers of 1.43 and 1.71 was obtained. The three swept wings had angles of sweep at 45, 55, and 63 degrees and were tested at a Mach number of 1.43.
Author: Edward Seckel Publisher: 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.
Author: Russell W. McDearmon Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 26
Book Description
Experimental values of the damping in roll at zero angle of attack of the Bell X-1E research airplane and various combinations of its components have been obtained at Mach numbers of 1.62, 1.04, 2.22, 2.41, and 2.62.
Author: United States. Superintendent of Documents Publisher: ISBN: Category : Government publications Languages : en Pages : 1714
Book Description
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.
Author: Russell W. McDearmon
Author: Russell W. McDearmon
Author: Macon C. Ellis
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: Edward Seckel
Author: United States. National Advisory Committee for Aeronautics
Author: A. Gerald Rainey
Author: Russell W. McDearmon
Author: United States. Superintendent of Documents
Author: