Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 202
Book Description
Large Scale Wind Tunnel Investigation of a Semispan Wing Equipped with an Externally-blown Jet Flap
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 202
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 202
Book Description
Large-scale Wind-tunnel Investigation of the Noise Characteristics of a Semispan Wing Equipped with an Externally Blown Jet Flap
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 240
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 240
Book Description
Wind-tunnel Investigation of a Large-scale Semispan Model with an Unswept Wing and an Upper-surface Blown Jet Flap
Author: Charles Christian Smith
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 156
Book Description
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 156
Book Description
Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap
Author: Jerry V. Kirk
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 400
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 400
Book Description
Prediction methods for jet V/STOL propulsion aerodynamics
Author: M. F. Platzer
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 548
Book Description
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 548
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 848
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 848
Book Description
Wind-tunnel Investigation of an External-flow Jet-flap Transport Configuration Having Full-span Triple-slotted Flaps
Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 276
Book Description
A wind-tunnel investigation has been conducted to determine the performance and static stability and control characteristics of an external-flow jet-flap transport configuration having inboard pod-mounted engines and full-span triple-slotted flaps. Tests were made with the engines mounted clustered at 22.0 percent and 30.4 percent semispan to represent double (Siamese) pods and with engines mounted at 22.0 percent and 41.7 percent semispan to represent a more spread arrangement. Tests were also made to evaluate the effectiveness of wing leading-edge blowing as a means of improving the aerodynamic efficiency of the configuration and of eliminating the large engine-out roll asymmetries that , occurred for the configuration when the wing with an engine out stalled first.
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 276
Book Description
A wind-tunnel investigation has been conducted to determine the performance and static stability and control characteristics of an external-flow jet-flap transport configuration having inboard pod-mounted engines and full-span triple-slotted flaps. Tests were made with the engines mounted clustered at 22.0 percent and 30.4 percent semispan to represent double (Siamese) pods and with engines mounted at 22.0 percent and 41.7 percent semispan to represent a more spread arrangement. Tests were also made to evaluate the effectiveness of wing leading-edge blowing as a means of improving the aerodynamic efficiency of the configuration and of eliminating the large engine-out roll asymmetries that , occurred for the configuration when the wing with an engine out stalled first.
Aeronautical Research and Development, Hearings Before the Subcommittee on Aeronautics and Space Technology..., 92-2, January 18, 19, and 20, 1972
Author: United States. Congress. House. Science and Astronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 960
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 960
Book Description