Publication Date:
2019-07-11
Description:
The 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.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-TM-1226
,
ZWB Der Luftfshrtforschung des Generalluftzeugmeisters Berlin-Adlershof, Untersuchungen und Mitteilungen Nr. 3176; Rept-3176
Format:
application/pdf
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