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Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topicsPublications prior to March 1981 were surveyed to determine inlet flow dynamic distortion prediction methods and to catalog experimental and analytical information concerning inlet flow dynamic distortion prediction methods and to catalog experimental and analytical information concerning inlet flow dynamics at the engine-inlet interface of conventional aircraft (excluding V/STOL). The sixty-five publications found are briefly summarized and tabulated according to topic and are cross-referenced according to content and nature of the investigation (e.g., predictive, experimental, analytical and types of tests). Three appendices include lists of references, authors, organizations and agencies conducting the studies. Also, selected materials summaries, introductions and conclusions - from the reports are included. Few reports were found covering methods for predicting the probable maximum distortion. The three predictive methods found are those of Melick, Jacox and Motycka. The latter two require extensive high response pressure measurements at the compressor face, while the Melick Technique can function with as few as one or two measurements.
Document ID
19830010458
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schweikhhard, W. G.
(Kansas Univ. Lawrence, KS, United States)
Chen, Y. S.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Publication Information
Publisher: NASA
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-3673
NAS 1.26:3673
Report Number: NASA-CR-3673
Report Number: NAS 1.26:3673
Accession Number
83N18729
Funding Number(s)
PROJECT: RTOP 505-32-12
CONTRACT_GRANT: NAG3-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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