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Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration


Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration
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Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration


Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration
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Author : Masashi Mizukami
language : en
Publisher:
Release Date : 2000

Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration written by Masashi Mizukami and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Airplanes categories.


A flat plate and faired pod have been mounted on a NASA SR-71A aircraft for use as a supersonic flight experiment test bed. A test article can be placed on the flat plate; the pod can contain supporting systems. A series of test flights has been conducted to validate this test bed configuration. Flight speeds to a maximum of Mach 3.0 have been attained. Steady-state sideslip maneuvers to a maximum of 2° have been conducted, and the flow field in the test region has been surveyed. Two total-pressure rakes, each with two flow-angle probes, have been placed in the expected vicinity of an experiment. Static-pressure measurements have been made on the flat plate. At subsonic and low supersonic speeds with no sideslip, the flow in the surveyed region is quite uniform. During sideslip maneuvers, localized flow distortions impinge on the test region. Aircraft sideslip does not produce a uniform sidewash over the test region. At speeds faster than Mach 1.5, variable-pressure distortions were observed in the test region. Boundary-layer thickness on the flat plate at the rake was less than 2.1 in. For future experiments, a more focused and detailed flow-field survey than this one would be desirable.



The Sr 71 Test Bed Aircraft A Facility For High Speed Flight Research


The Sr 71 Test Bed Aircraft A Facility For High Speed Flight Research
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Author : Stephen Corda
language : en
Publisher:
Release Date : 2000

The Sr 71 Test Bed Aircraft A Facility For High Speed Flight Research written by Stephen Corda and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Aerodynamics categories.


The SR-71 test bed aircraft is shown to be a unique platform to flight-test large experiments to supersonic Mach numbers. The test bed hardware mounted on the SR-71 upper fuselage is described. This test bed hardware is composed of a fairing structure called the "canoe" and a large "reflection plane" flat plate for mounting experiments. Total experiment weights, including the canoe and reflection plane, as heavy as 14,500 lb can be mounted on the aircraft and flight-tested to speeds as fast as Mach 3.2 and altitudes as high as 80,000 ft. A brief description of the SR-71 aircraft is given, including details of the structural modifications to the fuselage, modifications to the J58 engines to provide increased thrust, and the addition of a research instrumentation system. Information is presented based on flight data that describes the SR-71 test bed aerodynamics, stability and control, structural and thermal loads, the canoe internal environment, and reflection plane flow quality. Guidelines for designing SR-71 test bed experiments are also provided.



Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration


Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-13

Flow Field Survey In The Test Region Of The Sr 71 Aircraft Test Bed Configuration written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-13 with categories.


A flat plate and faired pod have been mounted on a NASA SR-71A aircraft for use as a supersonic flight experiment test bed. A test article can be placed on the flat plate; the pod can contain supporting systems. A series of test flights has been conducted to validate this test bed configuration. Flight speeds to a maximum of Mach 3.0 have been attained. Steady-state sideslip maneuvers to a maximum of 2 deg have been conducted, and the flow field in the test region has been surveyed. Two total-pressure rakes, each with two flow-angle probes, have been placed in the expected vicinity of an experiment. Static-pressure measurements have been made on the flat plate. At subsonic and low supersonic speeds with no sideslip, the flow in the surveyed region is quite uniform. During sideslip maneuvers, localized flow distortions impinge on the test region. Aircraft sideslip does not produce a uniform sidewash over the test region. At speeds faster than Mach 1.5, variable-pressure distortions were observed in the test region. Boundary-layer thickness on the flat plate at the rake was less than 2.1 in. For future experiments, a more focused and detailed flow-field survey than this one would be desirable. Mizukami, Masashi and Jones, Daniel and Weinstock, Vladimir D. Armstrong Flight Research Center RTOP 523-90-24



Flow Field Survey In The Test Region Of The Sr 17 Aircraft Test Bed Configuration


Flow Field Survey In The Test Region Of The Sr 17 Aircraft Test Bed Configuration
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Author : Masashi Mizukami
language : en
Publisher:
Release Date : 2000

Flow Field Survey In The Test Region Of The Sr 17 Aircraft Test Bed Configuration written by Masashi Mizukami and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2000 with Aerodynamics categories.




Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1993

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 1993 with Aeronautics categories.




The Finding Guide To Aiaa Meeting Papers


The Finding Guide To Aiaa Meeting Papers
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Author : American Institute of Aeronautics and Astronautics. Technical Information Service
language : en
Publisher:
Release Date : 1996

The Finding Guide To Aiaa Meeting Papers written by American Institute of Aeronautics and Astronautics. Technical Information Service and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with AIAA paper categories.




International Aerospace Abstracts


International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1999

International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.




Selected Water Resources Abstracts


Selected Water Resources Abstracts
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Author :
language : en
Publisher:
Release Date : 1984

Selected Water Resources Abstracts 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 Hydrology categories.




Government Research Directory


Government Research Directory
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Author : Cengage Gale
language : en
Publisher: Gale Cengage
Release Date : 2008-12

Government Research Directory written by Cengage Gale and has been published by Gale Cengage this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008-12 with Law categories.




Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1948

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Mechanics, Applied categories.