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On the Installation of Jet Engine Nacelles on a Wing Fourth Partial Report: Pressure-Distribution Measurements on a Sweptback Wing with Jet Engine NacelleThe present report, which deals with pressure-distribution measurements made on a sweptback wing with a jet engine nacelle, is similar to a report on pressure-distribution measurements on a rectangular wing with a jet engine nacelle (second partial report). Here, in investigations preliminary to high-speed measurements, as in the second partial report, useful arrangements and fillet designs have been discovered.
Document ID
20050029443
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Buschner, R.
(Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
July 1, 1949
Publication Information
Publication: ZWB Der Luftfshrtforschung des Generalluftzeugmeisters Berlin-Adlershof, Untersuchungen und Mitteilungen Nr. 3176
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-TM-1226
Report Number: NACA-TM-1226
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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