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Supersonic wings with significant leading-edge thrust at cruise (1980)

Carlson, H. W. ; Mack, R. J. ; Robins, A. W.

In: CASI

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Publication Date: 2019-06-27

Description: Experimental/theoretical correlations are presented which show that significant levels of leading-edge thrust are possible at supersonic speeds for certain planforms having the geometry to support the theoretical thrust-distribution potential. The new analytical process employed provides not only the level of leading-edge thrust attainable but also the spanwise distribution of both it and that component of full theoretical thrust which acts as vortex lift. Significantly improved aerodynamic performance in the moderate supersonic speed regime is indicated.

Keywords: AERODYNAMICS

Type: NASA-TP-1632 , L-13316

Format: application/pdf

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