Author: Robert F. PeckPublisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 32
Book Description
Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Having a 60 Degree Delta Wing and a High Unswept Horizontal Tail
Author: Robert F. PeckRocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail
Author: Robert F. PeckPublisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 32
Book Description
Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0
Author: John C. McFallPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37
Author: T. Bradley CurryPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
Book Description
Importants manuscrits et documents relatifs à la Bastille et au Faubourg Saint-Antoine
Author: Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-powered Model of a 60 Degrees Delta-wing Airplane from Mach Numbers of 0.75 to 1.70
Author: Grady L. MitchamResults of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-sided Fuselage
Author: Robert F. PeckPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26
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.
Applied Mechanics Reviews
Author: Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations
Author: Theodore J. GoldbergPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 108
Book Description
Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.
Effects of Wing Position and Vertical-tail Configuration on Stability and Control Characteristics of a Jet-powered Delta-wing Vertically Rising Airplane Model
Author: Powell M. LovellPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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.