Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail PDF Download
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Author: Robert F. Peck
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 32
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Book Description
Author: Robert F. Peck
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 32
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Book Description
Author: A. James Vitale
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Book Description
Author: Clement J. Welsh
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 15
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Book Description
Results of an exploratory free-flight investigation at zero-lift of several rocket-powered drag research models equipped with 60 degree swept-back delta wings are presented for a Mach number range from about 0.70 to 1.60. The airfoil sections tested included the NACA 65-006 and a series of double-wedge sections with various thicknesses and positions of maximum thickness.
Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
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Book Description
Author: Robert F. Peck
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: John B. McDevitt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
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Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author: Powell M. Lovell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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Book Description
An investigation has been conducted to determine the effects of wing position and vertical tail configuration on the stability and control characteristics of a jet-powered delta-wing vertically rising airplane model. A ducted-fan powerplant was used because there was no hot-jet powerplant of sufficiently small size and adequate reliability available. In addition to conventional flap-type control surfaces on the wings and vertical tails, the model had jet-reaction controls provided by movable eyelids at the rear of the tail pipe and by air bled from the main duct and exhausted through movable nozzles near the wing tips. The investigation consisted of flight and force tests of three model configurations: a high wing with a top-mounted vertical tail, a high wing with top- and bottom-mounted vertical tails, and a low wing with the top-mounted vertical tail. The flight tests, which were made in the Langley full-scale tunnel, represented slow constant-altitude transitions from hovering to normal unstalled forward flight.
Author: Dewey E. Wornom
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 30
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Book Description
