2012-2533 A Model-Based Approach to Engineering Behavior of Complex Aerospace Systems
A COMPARISON OF RESULTS OF PAK-3D WITH ANEXPERIMENTAL STUDY FOR A LOW - THRUST SATELLITE NOZZLE
A CONCEPTUAL DESIGN OF AN EJECTOR-FUEL CELL SYSTEM FOR SPACECRAFT APPLICATIONS
AIAA-2001-2479 Vorticity and its Transport in Juncture Flow
AIAA-2004-4732 Response of Vortex Breakdown Induced Wing Rock to Pitching & Plunging