Aeropropulsive Characteristics Of Mach Numbers Up To 2 2 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model

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Aeropropulsive Characteristics Of Mach Numbers Up To 2 2 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model

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Author : Francis J. Capone
language : en
Publisher:
Release Date : 1982

Aeropropulsive Characteristics Of Mach Numbers Up To 2 2 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model written by Francis J. Capone and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.

Nasa Technical Paper

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Author :
language : en
Publisher:
Release Date : 1984

Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Astronautics categories.

Nasa Technical Paper

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1977

Nasa Technical Paper written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Astronautics categories.

Nasa Scientific And Technical Publications

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Author :
language : en
Publisher:
Release Date : 1989

Nasa Scientific And Technical Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aeronautics categories.

Partners In Freedom

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Author : Joseph R. Chambers
language : en
Publisher:
Release Date : 2000

Partners In Freedom written by Joseph R. Chambers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Aeronautics, Military categories.

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.

Aeropulsive Characteristics At Mach Numbers Up To 2 2 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model

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Author : Francis J. Capone
language : en
Publisher:
Release Date : 1982

Aeropulsive Characteristics At Mach Numbers Up To 2 2 Of Axisymmetric And Nonaxisymmetric Nozzles Installed On An F 18 Model written by Francis J. Capone and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Jet nozzles categories.

An investigation to determine the aeropropulsive characteristics of nonaxisymmetric nozzles on an F-18 jet effects model was conducted in the Langley 16-foot transonic tunnel and the AEDC 16-foot supersonic wind tunnel. The performance of a two dimensional convergent-divergent nozzle, a single expansion ramp nozzle, and a wedge nozzle was compared with that of the baseline axisymmetric nozzle. Test data were obtained at static conditions and at Mach numbers from 0.60 to 2.20 at an angle of attack of 0 deg. Nozzle pressure ratio was varied from jet-off to about 20.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1987

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Aeronautics categories.

Nasa Technical Memorandum

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Author :
language : en
Publisher:
Release Date : 1989

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aeronautics categories.

Static Internal Performance Of A Single Expansion Ramp Nozzle With Multiaxis Thrust Vectoring Capability

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Author : Francis J. Capone
language : en
Publisher:
Release Date : 1993

Static Internal Performance Of A Single Expansion Ramp Nozzle With Multiaxis Thrust Vectoring Capability written by Francis J. Capone and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with categories.

Parametric Investigation Of Single Expansion Ramp Nozzles At Mach Numbers From 0 60 To 1 20

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Author : Francis J. Capone
language : en
Publisher:
Release Date : 1992

Parametric Investigation Of Single Expansion Ramp Nozzles At Mach Numbers From 0 60 To 1 20 written by Francis J. Capone and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aerodynamics categories.