A method for the continuous variation of the Mach number in a supersonic wind tunnel and some experimental results obtained at low supersonic speeds
By: Georg Drougge.
Contributors: Aeronautical Research Institute of Sweden
Series: Aeronautical Research Institute of Sweden. Report -- no. 29; Flygtekniska Forsoksanstalten. Meddelande -- nr. 29
Publisher: Aeronautical Research Institute of Sweden
Published: 1949
Place of publication: Stockholm
Number of pages: 14