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Sonic Boom Propagation Codes Validated by Flight TestThe sonic boom propagation codes reviewed in this study, SHOCKN and ZEPHYRUS, implement current theory on air absorption using different computational concepts. Review of the codes with a realistic atmosphere model confirm the agreement of propagation results reported by others for idealized propagation conditions. ZEPHYRUS offers greater flexibility in propagation conditions and is thus preferred for practical aircraft analysis. The ZEPHYRUS code was used to propagate sonic boom waveforms measured approximately 1000 feet away from an SR-71 aircraft flying at Mach 1.25 to 5000 feet away. These extrapolated signatures were compared to measurements at 5000 feet. Pressure values of the significant shocks (bow, canopy, inlet and tail) in the waveforms are consistent between extrapolation and measurement. Of particular interest is that four (independent) measurements taken under the aircraft centerline converge to the same extrapolated result despite differences in measurement conditions. Agreement between extrapolated and measured signature duration is prevented by measured duration of the 5000 foot signatures either much longer or shorter than would be expected. The duration anomalies may be due to signature probing not sufficiently parallel to the aircraft flight direction.
Document ID
19970011188
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Poling, Hugh W.
(Boeing Co. Seattle, WA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-201634
NAS 1.26:201634
Report Number: NASA-CR-201634
Report Number: NAS 1.26:201634
Accession Number
97N16198
Funding Number(s)
PROJECT: RTOP 537-07-21
CONTRACT_GRANT: NAS1-20220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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