2010Hangkong bingqiRequires access

Aerodynamic Characteristic of Missile and Pylon During the Aeroplane-Missile Inteference Effect

Ding Yu

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Abstract

This paper analyzes the variation of aerodynamic load with attack angle,slideslip angle,chordwish and spanwish location,and Mach,which is in the flow field below the wing.It is concluded that the aerodynamic characteristic of missile and pylon is usually decided by flight attitude and the location of missile and launcher.

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What this paper is about

This paper analyzes the variation of aerodynamic load with attack angle,slideslip angle,chordwish and spanwish location,and Mach,which is in the flow field below the wing.It is concluded that the aerodynamic characteristic of missile and pylon is usually decided by flight attitude and the location of missile and launcher.

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Available abstract

This paper analyzes the variation of aerodynamic load with attack angle,slideslip angle,chordwish and spanwish location,and Mach,which is in the flow field below the wing.It is concluded that the aerodynamic characteristic of missile and pylon is usually decided by flight attitude and the location of missile and launcher.

Key concepts: Missile, Aerodynamics, Mach number, Aerospace engineering, Pylon, Angle of attack, Engineering, Aeronautics

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