Browsing CoA. Notes (1952-1969) by Author "Busing, J. R."

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Experimental investigation of the interference of a body on a low aspect ratio wing of rectangular planform at a Mach number of 2

Busing, J. R.; Marson, G. B.; Lilley, G. M. (College of Aeronautics, 1955-06)

Results are given of pressure measurements on awing of gross aspect ratio approximately 2/3 mounted on a cylindrical body with an ogival nose, made at a Mach number of 2.00 in the 9in, x 9in, supersonic -wind tunnel at ...
A preliminary experimental investigation of the effect of surface catalytic efficiency on stagnation point heat transfer

Busing, J. R. (College of Aeronautics, 1962-01)

Results of an experimental investigation to measure the difference between the heat transfer rate to a catalytic wall and to a non-catalytic wall are presented. Using thin film thermometer techniques, associated with an ...
A preliminary investigation of the flow over a particular wing body combination at Mach number 2

Busing, J. R.; Lilley, G. M. (College of Aeronautics, 1955-04)

Results are presented of visual tests, by surface flow and Schlieren techniques, of the flaw over a particular wing body combination at M = 2.0, made in the 9in x 9in supersonic wind tunnel at the College of Aeronautics. ...

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