Collection of Test Data for Lateral Control with Full-span Flaps PDF Download
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Author: Jack Fischel
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 612
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Book Description
A collection of available test data on lateral control with full-span flaps is presented. The lateral-control effectiveness and hinge-moment data presented include the characteristics of spoiler devices and ailerons with retractable flaps. The basic data presented on the various flap and aileron combinations should facilitate the design of full-span-flap laterial-control arrangements. A discussion is given of the characteristics of the lateral-control devices considered and of the application of the data to specific airplane design.
Author: Jack Fischel
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 612
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Book Description
A collection of available test data on lateral control with full-span flaps is presented. The lateral-control effectiveness and hinge-moment data presented include the characteristics of spoiler devices and ailerons with retractable flaps. The basic data presented on the various flap and aileron combinations should facilitate the design of full-span-flap laterial-control arrangements. A discussion is given of the characteristics of the lateral-control devices considered and of the application of the data to specific airplane design.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 594
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 34
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Book Description
Author: Kenneth Margolis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 724
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Book Description
Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio, aspect ratio, sweepback, and Mach number are determined. Calculations are presented for representative plan forms and for a family of wings having equal root bending stress.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: Allen F. Donovan
Publisher: Princeton University Press
ISBN: 140087503X
Category : Science
Languages : en
Pages : 1021
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Book Description
Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 642
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Book Description
