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Design and development of an F/A-18 inlet distortion rake: A cost and time saving solutionAn innovative inlet total-pressure distortion measurement rake has been designed and developed for the F/A-18 A/B/C/D aircraft inlet. The design was conceived by NASA and General Electric Aircraft Engines (Evendale, Ohio). This rake has been flight qualified and flown in the F-18 High Alpha Research Vehicle (HARV) at NASA Dryden Flight Research Center. The rake's eight-legged, one-piece wagon wheel design was developed at a reduced cost and offers reduced installation time compared with traditional designs. The rake features 40 dual measurement ports for both low- and high-frequency pressure measurements with the high-frequency transducer mounted at the port. The high-frequency transducer offers direct absolute pressure measurements from low frequency to the highest frequency of interest, thereby allowing the rake to be used during highly dynamic aircraft maneuvers. Outstanding structural characteristics are inherent to the design through its construction and use of lightweight materials.
Document ID
19950007827
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yuhas, Andrew J.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Ray, Ronald J.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Burley, Richard R.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Steenken, William G.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Lechtenberg, Leon
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Thornton, Don
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: Fourth High Alpha Conference, Volume 2 17 p(SEE N95-14239 03-02)
Subject Category
Aerodynamics
Accession Number
95N14241
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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