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Three-Component Force and Mass-Flow Measurement on a Jet NacelleThe present report contains three-component forces and mass-flow measurements on a jet nacelle at small inlet-velocity ratios v(sub A)/v(sub o) < 1. The mass-flow measurement on two cross sections of the nacelle demonstrate the local-velocity distribution with varying flow and angle of attack.
Document ID
20030064188
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Ilgmann, G.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Moeller, E.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 1947
Subject Category
Aerodynamics
Report/Patent Number
NACA-TM-1149
Report Number: NACA-TM-1149
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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