J. E. DANBERG

Navier-Stokes Computations of Transonic Flow Over a Projectile with a Two-Equation Model of Turbulence, (9999)

Sahu,J., Danberg,J. E.

A thin-layer Navier-Stokes code has been used to compute the axisymmetric turbulent flow over a projectile at transonic speeds. The thin layer form of the compressible Navier-Stokes equations is...

Transonic Pressure Distribution and Boundary Layer Characteristics of a Projectile with an Asymmetric Afterbody. (2002)

Danberg,J. E., Tschirschnitz,R. H.

Measurements of pressure distribution and boundary layer characteristics were obtained on an asymmetric boattail projectile. Such configurations are being studied as potential alternatives to...

Computational Simulation of Transonic Flow Over Projectile Rotating Band and Comparison with Experiment. (2002)

Danberg,J. E., Heavey,K. R., Miller,M. C.

An azimuthal-invarient Navier-Stokes computational method is used to predict the transonic (M = 0.94) flow field about an artillery shell with and without a simulated rotating band. The pressure...

Modified Point Mass Trajectory Simulation for Base-Burn Projectiles (2002)

Lieske, R. F., Danberg, J. E.

An addition to the Modified Point Mass Trajectory Model for Rocket- Assisted Projectiles is presented for the exterior ballistic simulation of base- bum projectiles. The addition models the change in...

HEAT-TRANSFER CHARACTERISTICS OF A HEMISPHERE CYLINDER AT HYPERSONIC MACH NUMBERS (1998)

WINKLER, E.M., DANBERG, J.E.