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Altitude-Wind-Tunnel Tests of Power-Plant Installation in Jet-Propelled Fighter
Document ID
19930092672
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jagger, James M
Date Acquired
August 15, 2013
Publication Date
February 1, 1946
Report/Patent Number
NACA-MR-E5L17
NACA-WR-E-274
Report Number: NACA-MR-E5L17
Report Number: NACA-WR-E-274
Accession Number
93R21962
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES-BELL P-59A (WIND TUNNEL TESTS-AERL - TURBOJET - HIGH-ALTITUDE) (AMER )
AIR FLOW - DUCTS
ENGINES - GENERAL ELECTRIC I-16 TURBOJET (WIND TUNNEL TESTS-AERL-HIGH-ALTITUDE)(
PRESSURE DISTRIBUTION - ENGINE NACELLES - BELL P-59A
ENGINE NACELLES, TURBOJET
BELL P-59A WIND TUNNEL TESTS (AERL-HIGH ALTITUDE)
BOUNDARY LAYER REMOVAL
AIR FLOW - ENGINE NACELLES
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