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TCA High Lift Preliminary AssessmentThis paper presents a TCA (Technology Concept Airplane) High lift Preliminary Assessment. The topics discussed are: 1) Model Description; 2) Data Repeatability; 3) Effect of Inboard L.E. (Leading Edge) Flap Span; 4) Comparison of 14'x22' TCA-1 With NTF (National Transonic Facility) Modified Ref. H; 5) Comparison of 14'x22' and NTF Ref. H Results; 6) Effect of Outboard Sealed Slat on TCA; 7) TCA Full Scale Build-ups; 8) Full Scale L/D Comparisons; 9) TCA Full Scale; and 10) Touchdown Lift Curves. This paper is in viewgraph form.
Document ID
20000036434
Document Type
Conference Paper
Authors
Wyatt, G. H. (Boeing Co. Seattle, WA United States)
Polito, R. C. (Boeing Co. Seattle, WA United States)
Yeh, D. T. (Boeing Co. Seattle, WA United States)
Elzey, M. E. (Boeing Co. Seattle, WA United States)
Tran, J. T. (Boeing Co. Seattle, WA United States)
Meredith, Paul T. (Boeing Co. Seattle, WA United States)
Date Acquired
September 8, 2013
Publication Date
December 1, 1999
Publication Information
Publication: 1998 NASA High-Speed Research Program Aeodynamic Performance Workshop
Volume: 2
Subject Category
Aerodynamics
Funding Number(s)
CONTRACT_GRANT: NAS1-20220
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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