TCA High Lift Preliminary Assessment

Authors :: Wyatt, G. H
Polito, R. C
Yeh, D. T
Elzey, M. E
Tran, J. T
Meredith, Paul T
Source :: 1998 NASA High-Speed Research Program Aeodynamic Performance Workshop. 2
Publication Year :: 1999
Publisher :: United States: NASA Center for Aerospace Information (CASI), 1999.
Abstract: This 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.

Language :: English
Volume :: 2
Database :: NASA Technical Reports
Journal :: 1998 NASA High-Speed Research Program Aeodynamic Performance Workshop
Notes :: NAS1-20220
Publication Type :: Report
Accession number :: edsnas.20000036434
Document Type :: Report

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