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F-15 inlet/engine test techniques and distortion methodologies studies. Volume 4: Autocorrelation functionsAutocorrelation function plots were used to determine if peak distortion data taken from a subscale inlet model can be used to predict peak distortion levels for a full scale flight test vehicle.
Document ID
19780022183
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stevens, C. H. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Spong, E. D. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Hammock, M. S. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-144869
Report Number: NASA-CR-144869
Accession Number
78N30126
Funding Number(s)
PROJECT: RTOP 514-54-04
CONTRACT_GRANT: NAS4-2364
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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