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Stability and performance characteristics of a fixed arrow wing supersonic transport configuration (SCAT 15F-9898) at Mach numbers from 0.60 to 1.20Tests on a 0.015 scale model of a supersonic transport were conducted at Mach numbers from 0.60 to 1.20. Tests of the complete model with three wing planforms, two different leading-edge radii, and various combinations of component parts, including both leading- and trailing-edge flaps, were made over an angle-of-attack range from about -6 deg to 13 deg and at sideslip angles of 0 deg and 2 deg.
Document ID
19780022144
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Decker, J. P. (NASA Langley Research Center Hampton, VA, United States)
Jacobs, P. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-78726
Report Number: NASA-TM-78726
Accession Number
78N30087
Funding Number(s)
PROJECT: RTOP 743-04-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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