A program for the prediction of stationary subsonic flow about airplane configurations; a user's guide for the NLR-panel method

TL;DRAbstract

This report describes the use of the NLR-panel method program, for the computation of aerodynamic characteristics of bodies in stationary subsonic flow at a number of angles of attack. A short description of method and program, as well as a detailed description of input and output is presented. A program list (microfiche) and an example of related input and output (microfich are included).

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