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: Robert F. Peck
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: John C. McFall
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
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Book Description
Author: T. Bradley Curry
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: Robert F. Peck
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26
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Book Description
A rocket-propelled model of an airplane configuration having an arrow wing with 55 degree leading-edge sweep and a flat-sided fuselage mounting swept horizontal and vertical tails has been tested through use of the pulse-control technique at Mach numbers between 1.0 and 2.3. Results are presented from an investigation of longitudinal trim, lift, stability, drag, lateral force, thrust, and jet effects.
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:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1116
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Book Description
Author: Theodore J. Goldberg
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 108
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Book Description
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.
Author: Bernard Spencer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
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Book Description
