Aerodynamic design of two dimensional supersonic nozzle contours with boundary layer corrections

Satyanarayana, B and Irani, PA (1961) Aerodynamic design of two dimensional supersonic nozzle contours with boundary layer corrections. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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Abstract

Various methods of determining supersonic aerodynamic nozzle contours are presented. The aerodynamic contours their slcpes and curvatures are calculated both by the graphical as well as Poelsch's methods. The displacement thickness Is determined on the side walls and contour waiis and the aerodyiiaxic contours corrected for boundary layeyer effects are presented.

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Supersonic;Aerodynamic nozzle;Poelsch's methods
Subjects: AERONAUTICS > Aerodynamics
Depositing User: M/S ICAST NAL
Date Deposited: 19 Dec 2006
Last Modified: 08 Jan 2021 12:10
URI: http://nal-ir.nal.res.in/id/eprint/3781

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