Computations of supersonic vortical flows around ogive-cylinders using central and upwind differences /
Eswar Josyula.

Description

Main Author

Josyula, Eswar

Related Names

Wright Laboratory (Wright-Patterson Air Force Base, Ohio)

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate, Wright Laboratory, Air Force Materiel Command, United States Air Force, 1997.

Subjects

Guided missiles > Guided missiles / Aerodynamics.
Aerodynamics, Supersonic.
Computational fluid dynamics.
Whirlwinds.

Summary

This work is part of a cooperative research, development, test and evaluation program that brings scientists and engineers from various English-speaking countries together for collaborative studies to improve technology to solve technical problems. The current TTCP work project WTP-2 KTA 2-12, 'Application of CFD to the prediction of Missile Body Vortices' focuses on the ability of the three-dimensional Navier-Stokes equations to predict flowfields about high length-to-diameter bodies at moderate angles of attack (8 deg

Note

"Final report for 1 July 1994 - 1 March 1996."
"March 1997."

Physical Description

xii, 39 pages : illustrations ; 28 cm.

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