Wind-tunnel Investigation of an External-flow Jet-flap Transport Configuration Having Full-span Triple-slotted Flaps

Wind-tunnel Investigation of an External-flow Jet-flap Transport Configuration Having Full-span Triple-slotted Flaps PDF Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 276

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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.

Wind-tunnel Investigation of an External-flow Jet-flap Transport Configuration Having Full-span Triple-slotted Flaps

Wind-tunnel Investigation of an External-flow Jet-flap Transport Configuration Having Full-span Triple-slotted Flaps PDF Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 276

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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.

Wind-tunnel Investigation of a Large 35 ̊swept-wing Jet Transport Model with an External-flow Jet-augmented Double-slotted Flap

Wind-tunnel Investigation of a Large 35 ̊swept-wing Jet Transport Model with an External-flow Jet-augmented Double-slotted Flap PDF Author: Kiyoshi Aoyagi
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 84

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Wind tunnel tests of swept wing jet transport aircraft model with four pod mounted engines under wing and external flow, jet augmented double slotted flap.

Wind-tunnel Investigation of a Large Jet Transport Model Equipped with an External-flow Jet Flap

Wind-tunnel Investigation of a Large Jet Transport Model Equipped with an External-flow Jet Flap PDF Author: Lysle P. Parlett
Publisher:
ISBN:
Category : Jet flaps (Airplanes)
Languages : en
Pages : 90

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 464

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

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Partners in Freedom

Partners in Freedom PDF Author: Joseph R. Chambers
Publisher:
ISBN:
Category : Aeronautics, Military
Languages : en
Pages : 280

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Book Description
Established in 1917 as the nation#s first civil aeronautics research laboratory under the National Advisory Commit-tee for Aeronautics (NACA), Langley was a small laboratory that solved the problems of flight for military and civil aviation. Throughout history, Langley has maintained a working partnership with the Department of Defense, U.S. industry, universities, and other government agencies to support the defense of the nation with research. During World War II, Langley directed virtually all of its workforce and facilities to research for military aircraft. Following the war, a balanced program of military and civil projects was undertaken. In some instances Langley research from one aircraft program helped solve a problem in another. At the conclusion of some programs, Langley obtained the research models for additional tests to learn more about previously unknown phenomena. The data also proved useful in later developmental programs. Many of the military aircraft in the U.S. inventory as of late 1999 were over 20 years old. Langley activities that contributed to the development of some of these aircraft began over 50 years prior. This publication documents the role, from early concept stages to problem solving for fleet aircraft, that Langley played in the military aircraft fleet of the United States for the 1990's.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494

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