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Full Potential and Euler solutions for transonic unsteady flow

Published online by Cambridge University Press:  04 July 2016

D. Ambrosi ,
L. Gasparini  and
L. Vigevano
D. Ambrosi
Affiliation:
Dipartimento di Ingegneria Aerospaziale Politecnico di Milano, Italy
L. Gasparini
Affiliation:
Dipartimento di Ingegneria Aerospaziale Politecnico di Milano, Italy
L. Vigevano
Affiliation:
Dipartimento di Ingegneria Aerospaziale Politecnico di Milano, Italy
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Abstract

A comparison between Full Potential and Euler numerical solutions for 2D transonic unsteady flow is presented. The pros and cons of the potential model are discussed and the main features of both computational methods are summarised. The comparison is done for a Naca 0012 aerofoil oscillating in pitch at a freestream Mach number ranging from 0·755 to 0·825, in order to investigate the limit of application of the potential approximation in an unsteady flow.

Type
Research Article
Information
The Aeronautical Journal , Volume 98 , Issue 979 , November 1994 , pp. 340 - 348
Copyright
Copyright © Royal Aeronautical Society 1994 

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