Flight Test Results from the Rake Airflow Gage Experiment on the F-15b Airplane PDF Download
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Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781793962935
Category : Science
Languages : en
Pages : 34
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Book Description
The Rake Airflow Gage Experiment involves a flow-field survey rake that was flown on the Propulsion Flight Test Fixture at the NASA Dryden Flight Research Center using the Dryden F-15B research test bed airplane. The objective of this flight test was to ascertain the flow-field angularity, local Mach number profile, total pressure distortion, and dynamic pressure at the aerodynamic interface plane of the Channeled Centerbody Inlet Experiment. This new mixed-compression, supersonic inlet is planned for flight test in the near term. Knowledge of the flow-field characteristics at this location underneath the airplane is essential to flight test planning and computational modeling of the new inlet, an
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781793962935
Category : Science
Languages : en
Pages : 34
Get Book Here
Book Description
The Rake Airflow Gage Experiment involves a flow-field survey rake that was flown on the Propulsion Flight Test Fixture at the NASA Dryden Flight Research Center using the Dryden F-15B research test bed airplane. The objective of this flight test was to ascertain the flow-field angularity, local Mach number profile, total pressure distortion, and dynamic pressure at the aerodynamic interface plane of the Channeled Centerbody Inlet Experiment. This new mixed-compression, supersonic inlet is planned for flight test in the near term. Knowledge of the flow-field characteristics at this location underneath the airplane is essential to flight test planning and computational modeling of the new inlet, an
Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289169831
Category :
Languages : en
Pages : 36
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Book Description
The Rake Airflow Gage Experiment involves a flow-field survey rake that was flown on the Propulsion Flight Test Fixture at the NASA Dryden Flight Research Center using the Dryden F-15B research test bed airplane. The objective of this flight test was to ascertain the flow-field angularity, local Mach number profile, total pressure distortion, and dynamic pressure at the aerodynamic interface plane of the Channeled Centerbody Inlet Experiment. This new mixed-compression, supersonic inlet is planned for flight test in the near term. Knowledge of the flow-field characteristics at this location underneath the airplane is essential to flight test planning and computational modeling of the new inlet, an
Author: Michael A. Frederick
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721526345
Category :
Languages : en
Pages : 32
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Book Description
Flights of the F-15B/Propulsion Flight Test Fixture (PFTF) with a Cone Drag Experiment (CDE) attached have been accomplished at NASA Dryden Flight Research Center. Mounted underneath the fuselage of an F-15B airplane, the PFTF provides volume for experiment systems and attachment points for propulsion experiments. A unique feature of the PFTF is the incorporation of a six-degree-of-freedom force balance. The force balance mounts between the PFTF and experiment and measures three forces and moments. The CDE has been attached to the force balance for envelope expansion flights. This experiment spatially and inertially simulates a large propulsion test article. This report briefly describes the F-15B airplane, the PFTF, and the force balance. A detailed description of the CDE is provided. Force-balance ground testing and stiffness modifications are described. Flight profiles and selected flight data from the envelope expansion flights are provided and discussed, including force-balance data, the internal PFTF thermal and vibration environment, a handling qualities assessment, and performance capabilities of the F-15B airplane with the PFTF installed. Palumbo, Nathan and Moes, Timothy R. and Vachon, M. Jake Armstrong Flight Research Center NASA/TM-2002-210736, NAS 1.15:210736, H-2507
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 58
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Book Description
Author: Russel M. Herrington
Publisher: Lulu.com
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 480
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Book Description
n the late 1940¿s and early 50¿s, planes flew higher and faster than anyone had dreamed possible. The jet age had arrived, and along with it came turbojet and rocket-powered aircraft capable of flying beyond the speed of sound. To assess these aircraft, the Air Research and Development Command developed a series of data reduction methods, and then compiled them in this Flight Test Engineering Manual. It served as a standard technical reference for the flight test engineers, program managers, pilots and support teams for many of the X-plane programs of the 1950s. This reprint represents the first time in over fifty years that this book has been available, and the first time it has ever been made available to the public. it¿s a unique time capsule that provides insight into the era of ¿The Right Stuff¿, when slide rules and punch cards were the cutting edge, and a must-have for anyone interested in the technical aspects of flight test.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1026
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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.
Author: Wendell H. Stillwell
Publisher:
ISBN:
Category : X-15 (Rocket aircraft).
Languages : en
Pages : 140
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Book Description
Author: Albert C. Piccirillo
Publisher:
ISBN: 9781626830226
Category : Airplanes, Military
Languages : en
Pages : 328
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Book Description
Author: Joseph R. Chambers
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 406
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Book Description
