The high angle of attack data was analyzed to deduce the vortex shedding location, the vortex strength, and the vortex paths in the wake. Pdf high angleofattack hypersonic aerodynamics researchgate. High angle of attack aerodynamic predictions using missile. High angle of attack missile aerodynamics including rotational rates program m3hax. A large body of wind tunnel data was generated by tests of a smooth missile modcel with. The missile coordinate frame m frame and a frame parallel to the m frame were used for aerodynamics to allow convenient simulation of either the. The high angle of attack d3ta was analyzed to deduce the vortex.
This document presents equations for aerodynamic forces and moments to be used in 6dof missile simulations such as maveric. The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perf. High angle of attack aerodynamics available for download and read online in other formats. Pdf high angle of attack aerodynamics sravankumar kota.
American institute of aeronautics and astronautics 12700 sunrise valley drive, suite 200 reston, va 201915807 703. The present status and the future of missile aerodynamics. Pdf a preliminary design aerodynamics force model has been. High angle of attack aerodynamic predictions using missile datcom. Cronvich missile aerodynamics prefer to locate the air inlets. High angleofattack aerodynamics is increasing in importance because of the demand for. Download pdf high angle of attack aerodynamics book full free. In the six years since the last agard meeting on missile aerodynamics in. Panel methods for aircraft and missile configurations at high angles of attack 177 7. Discrete vortex theory was examined as a method which could be modified, based on experimental data, and used to predict the aerodynamic characteristics of missiles to greater accuracy. Mountain view, ca 94043 abstract s reference area the engineeringlevel missile aerodynamic prediction included angle of attack.
387 1666 1281 1608 176 942 1268 849 294 723 1384 1571 100 799 528 475 63 604 1681 43 1369 1087 111 730 1259 1660 290 370 1278 756 279 220 584 617 339 780 171 33 1326