Sting and Jet Interference Effects on the Afterbody Drag of a Twin-engine Variable Sweep Fighter Model at Transonic Speeds

Sting and Jet Interference Effects on the Afterbody Drag of a Twin-engine Variable Sweep Fighter Model at Transonic Speeds PDF Author:
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ISBN:
Category :
Languages : en
Pages : 76

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 910

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Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va

Proceedings of NASA Conference on Supersonic-Transport Feasibility Studies and Supporting Research, September 17-19, 1963, Langley Research Center, Langley Station, Hampton, Va PDF Author:
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ISBN:
Category : Supersonic transport planes
Languages : en
Pages : 528

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 140

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NASA Technical Paper

NASA Technical Paper PDF Author:
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ISBN:
Category : Astronautics
Languages : en
Pages : 244

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Jet Exit and Airframe Interference Studies on Twin-engine-fuselage Aircraft Installations

Jet Exit and Airframe Interference Studies on Twin-engine-fuselage Aircraft Installations PDF Author:
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Category :
Languages : en
Pages : 28

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Jet exhaust and support interference effects on the transonic aerodynamic characteristics of a fighter model with two widely spaced engines

Jet exhaust and support interference effects on the transonic aerodynamic characteristics of a fighter model with two widely spaced engines PDF Author: William B. Compton
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144

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A Summary of Research on Variable-sweep Fighter Airplanes

A Summary of Research on Variable-sweep Fighter Airplanes PDF Author:
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Category :
Languages : en
Pages : 84

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Partners in Freedom

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

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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.

Exhaust-nozzle Characteristics for a Twin-jet Variable-wing-sweep Fighter Airplane Model at Mach Numbers to 2.2

Exhaust-nozzle Characteristics for a Twin-jet Variable-wing-sweep Fighter Airplane Model at Mach Numbers to 2.2 PDF Author: David E. Reubush
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 148

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