APPLICATION OF EULER AND NAVIER-STOKES CODES TO MISSILE TYPE BODIES WITH HIGH L/D RATIOS

Authors
  1. Jones, D.J.
  2. Evans, J.
  3. Priolo, F.J.
  4. Sturek, W.B.
  5. Wardlaw, A.B.
Corporate Authors
Institute for Aerospace Research, Ottawa ONT (CAN);Defence Research Establishment Valcartier, Valcartier QUE (CAN);Naval Surface Warfare Center, Silver Spring MD (US);Army Ballistic Research Lab, Aberdeen Proving Ground MD (US)
Abstract
Several Euler codes and a Parabolised Navier-Stokes code are used to predict normal forces, pitching moments and centres of pressure on long axisymmetric bodies which are cone cylinders or tangent ogive cylinders one of which has 3 fins. Only supersonic flow situations are considered so that downstream marching methods are valid. The Mach number range is from 2 to 5 and the incidence range is up to 15 degrees.
Report Number
AGARD-CP-493-PAP-8 — @Paper presented at the Symposium of the Fluid Dynamics Panel, Friedrichshafen, West Germany, 23-26 April 1990; CONTAINED IN 91-02972
Date of publication
15 Oct 1990
Number of Pages
15
DSTKIM No
91-02964
CANDIS No
70158
Format(s):
Originator's fiche received by DSIS

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