Angle-of-attack motion of a spinning entry vehicle.
Angle of attack effect on motion throughout entry of spinning descending vehicle, noting effects of transverse angular velocity and spin rate
Engineering topics
Publications and source records attributed to Prislin, R. H..
Angle of attack effect on motion throughout entry of spinning descending vehicle, noting effects of transverse angular velocity and spin rate
Solution for angular motion analysis on spinning atmospheric entry vehicle
Tricyclic equation of motion extended because of importance increase of nonplanar free flight testing
Aerodynamic damping coefficient from wind tunnel free flight trajectories of nonaxisymmetrical bodies
High amplitude, dynamic stability characteristics of blunt 10-degree cones
Wind tunnel free-flight testing of reentry vehicle dynamics, noting capability for simultaneous two- dimensional viewing of model trajectories
Wind tunnel test of dynamic stability characteristics of spherically blunted 10 degree cones
Free flight dynamic stability measurements indicate that boundary layer transition has no perceptible effect
Free flight and free oscillation methods for wind tunnel dynamic stability testing