Publication Date:
2019-07-13
Description:
An 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 personnel. This rake has been flight qualified and flown in the F/A-18 High Alpha Research Vehicle at NASA Dryden Flight Research Center, Edwards, California. The eight-legged, one-piece, wagon wheel design of the rake was developed at a reduced cost and offered reduced installation time compared to traditional designs. The rake features 40 dual-measurement ports for low- and high-frequency pressure measurements with the high-frequency transducer mounted at the port. This high-frequency transducer offers direct absolute pressure measurements from low to high frequencies 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.
Keywords:
AERODYNAMICS
Type:
NASA-TM-4722
,
NAS 1.15:4722
,
H-2078
,
AIAA PAPER 94-2132
,
NIPS-95-05907
,
Biennial AIAA Flight Test Conference; Jun 20, 1994 - Jun 23, 1994; Colorado Springs, CO; United States
Format:
application/pdf
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