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Wind-Tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan FormsWind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-forward, and yawed wings. Tests covered changes in aspect ratio, taper ratio, and tip shape.
Document ID
20030064944
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Purser, Paul E. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Spearman, M. Leroy (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 21, 2013
Publication Date
May 22, 1947
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L7D23
Report Number: NACA-RM-L7D23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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