Abstract
In order to compute the aerodynamic characteristic of an Air-to-air Missile in different mach numbers and different attack angles were carried though making use of CFD software Fluent, the 3-D Reynolds-averaged incompressible Navier-Stokes equations were solved numerically by using a finite volume method. The movement trend of pitching moment coefficient, lift coefficient, and drag coefficient with variety of mach numbers and attack angles were gained, meanwhile, distributing trends of pressure, temperature and airflow velocity were also obtained. The results indicated that the basis and references could be offered by numerical computation results for shape design of missile and definite preponderances were showed than traditionary numerical computation methods.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
