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Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurationsTwo 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were tested at Mach numbers from 0.60 to 2.70. One model incorporated a varying dihedral (swept-up) wing to obtain the desired lateral-directional characteristics; the other incorporated more conventional twin vertical tails. The data from the wind-tunnel tests are presented without analysis.
Document ID
19790011891
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dollyhigh, S. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
L-12426
NASA-TM-78764
Report Number: L-12426
Report Number: NASA-TM-78764
Accession Number
79N20062
Funding Number(s)
PROJECT: RTOP 517-53-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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