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Recent flight-test results of optical airdata techniquesOptical techniques for measuring airdata parameters were demonstrated with promising results on high performance fighter aircraft. These systems can measure the airspeed vector, and some are not as dependent on special in-flight calibration processes as current systems. Optical concepts for measuring freestream static temperature and density are feasible for in-flight applications. The best feature of these concepts is that the air data measurements are obtained nonintrusively, and for the most part well into the freestream region of the flow field about the aircraft. Current requirements for measuring air data at high angle of attack, and future need to measure the same information at hypersonic flight conditions place strains on existing techniques. Optical technology advances show outstanding potential for application in future programs and promise to make common use of optical concepts a reality. Results from several flight-test programs are summarized, and the technology advances required to make optical airdata techniques practical are identified.
Document ID
19940009318
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bogue, Rodney K.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-4504
H-1915
SAE-92-1997
NAS 1.15:4504
Report Number: NASA-TM-4504
Report Number: H-1915
Report Number: SAE-92-1997
Report Number: NAS 1.15:4504
Meeting Information
Meeting: SAE Aerotech 1992
Location: Anaheim, CA
Country: United States
Start Date: October 5, 1992
End Date: October 8, 1992
Accession Number
94N13791
Funding Number(s)
PROJECT: RTOP 505-68-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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