Previous (E36: Dynamic Overset Grid Demonstration Using A Simple Rotor/Fuselage Model) | Up | Next (E38: Time-Dependent Oscillating Flap Demonstration)

Application #37. Hypersonic Tethered Ballute Simulation

Contributed by Rena Rudavsky, summer student from Columbia University

Simulation of viscous flow over a tethered ballute configuration, based on a parametric model constructed with Pro/E and gridded with GridEx/AFLR3. One quarter of the domain is simulated, implying a 4-tether ballute arrangement. Performed at 8.55 km/sec using nitrogen.

Previous (E36: Dynamic Overset Grid Demonstration Using A Simple Rotor/Fuselage Model) | Up | Next (E38: Time-Dependent Oscillating Flap Demonstration)

NASA Official: David P. Lockard
Contact: FUN3D-support@lists.nasa.gov
Page Last Modified: 2024-04-25 10:30:27 -0400
NASA Privacy Statement
Accessibility

This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States.