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• W1569429452 abstract "NASA-Lewis has conducted wind tunnel experiments to ascertain the effectiveness of state-of-the-art in natural laminar flow (NLF) and LFC airfoils for subsonic and transonic speeds, such as the NLF(1)-0414F and the SCLFC(1)-0513F. Attention is given to the effects of Tollmien-Schlichting (TS) and/or crossflow linear mechanisms amplifying small disturbances to generate turbulence. It is found that the incompressible TS transitional n-factors were generally in the 9-12 range, in agreement with earlier correlation studies; the TS instability was the dominant instability mode on a swept-planform LFC airfoil over the entire range of test conditions." @default.
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• W1569429452 date "1987-10-01" @default.
• W1569429452 modified "2023-09-23" @default.
• W1569429452 title "Boundary-Layer Stability Analysis of NLF and LFC Experimental Data at Subsonic and Transonic Speeds" @default.
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• W1569429452 doi "https://doi.org/10.4271/871859" @default.
• W1569429452 hasPublicationYear "1987" @default.
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