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The 727/JT8D refan side nacelle airloadsAirloads on the 727/JT8D refan side engine nacelle are presented. These consist of surface static pressure distributions from two low speed wind tunnel tests. External nacelle surface pressures are from testing of a flow-through, body mounted nacelle model, and internal inlet surface pressures are from performance testing of a forced air inlet model. The method for obtaining critical airloads on nacelle components and a representative example are discussed.
Document ID
19740018323
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bailey, R. W.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Vadset, H. J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-CR-134547
D6-41527
Report Number: NASA-CR-134547
Report Number: D6-41527
Accession Number
74N26436
Funding Number(s)
CONTRACT_GRANT: NAS3-17842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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