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Aerodynamic characteristics of a tandem wing configuration of a Mach number of 0.30An investigation was conducted to determine the aerodynamic characteristics of a tandem wing configuration. The configuration had a low forward mounted sweptback wing and a high rear mounted sweptforward wing jointed at the wing tip by an end plate. The investigation was conducted at a Mach number of 0.30 at angles of attack up to 20 deg. A comparison of the experimentally determined drag due to lift characteristics with theoretical estimates is also included.
Document ID
19760002978
Document Type
Technical Memorandum (TM)
Authors
Henderson, W. P. (NASA Langley Research Center Hampton, VA, United States)
Huffman, J. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
AERODYNAMICS
Report/Patent Number
NASA-TM-X-72779
Funding Number(s)
PROJECT: RTOP 505-11-21-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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