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pro vyhledávání: '"Antti Pankkonen"'
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
A generic split-canard air-to-air missile was simulated at angles of attack up to 60 degrees in turbulent subsonic flow using open source CFD software package OpenFOAM. The results were compared with aerodynamic data from wind tunnel experiments of t
Autor:
Antti Pankkonen
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
In previous work a high-order panel method was found to be a feasible tool for rapid aerodynamic modelling of missiles within preliminary design accuracy. The present paper addresses some issues identified within that work in an attempt to expand the
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
The High-g Barrel (HGB) roll as an aircraft avoidance maneuver against an air-to-air interceptor missile is revisited 1 . The objective of this paper is to study the capability of simplified methods to predict the end-game miss distance. In the first
Autor:
Antti Pankkonen
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
A high-order panel method is applied to compute longitudinal aerodynamic characteristics of several missile configurations for which wind-tunnel test data are available. Feasibility and limitations of the panel method in missile aerodynamic modelling