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Jet Diffusion in Proximity of a WallWhen auxiliary jet engines are installed on airframes; as well as in some new designs, the jet engines are mounted in such a way that the jet stream exhausts in close proximity to the fuselage. This report deals with the behavior of the jet in close proximity to a two-dimensional surface. The experiments were made to find out whether the axially symmetric stream tends to approach the flat surface. This report is the last of a series of four partial test reports of the Goettingen program for the installation of jet engines, dated October 12, 1943. This report is the complement of the report on intake in close proximity to a wall.
Document ID
20050031099
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Kuechemann, D.
(Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
May 1, 1949
Publication Information
Publication: Untersuchungen und Mitteilungen
Issue: 3057
Subject Category
Aerodynamics
Report/Patent Number
NACA-TM-1214
Report Number: NACA-TM-1214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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