A combined experimental and numerical study was conducted on a generic projectile
configuration with low-aspect-ratio fins. The main objectives of this study were to …

View Video Presentation: https://doi. org/10.2514/6.2022-0419. vid Several aerodynamic
databases are combined to form an aerodynamic model for a high-speed, longrange …

View Video Presentation: https://doi. org/10.2514/6.2022-0420. vid Several methods are
applied to capture the roll-dependent aerodynamics of a high-speed missile. An inviscid …

View Video Presentation: https://doi. org/10.2514/6.2022-0612. vid In this paper, we present
an approach to flight control design for guided projectile applications with expanded flight …

View Video Presentation: https://doi. org/10.2514/6.2023-3677. vid An experimental study
was conducted on an axisymmetric body with fins using pressure sensitive paint to acquire …

In this investigation, we simulated and analyzed several configurations of generic high-
speed test vehicle with control effectors in the shape of rectangular prisms. The performance …

Free flight experiments of projectiles have long been regarded as superior to wind tunnel
tests in estimating aerodynamic coefficients since realistic flight conditions are achieved and …

View Video Presentation: https://doi. org/10.2514/6.2022-1794. vid A methodology is
presented to analyze the performance characteristics of a marginally stable projectile with …

In the early stages of a new munition design process, it is desirable to quickly update the
controller as the aerodynamics and mass properties evolve. This allows for timely evaluation …