SUBSTR: 6-DOF store separation analysis for subsonic speeds. Aircraft components include fuselage, wings and up to three pylons, fixed stores. Stores with up to two finned sections, vortical wing-tail interference, specified ejection forces, specified thrust/time history, rail launch. Based on panel methods and slender body theory/reverse flow theorems.
HASLSB SUBSTR extended to handle rail launch from pitching aircraft at high angle of attack.
SUPSTR 6-DOF store separation analysis for supersonic speeds. Aircraft components include fuselage, wings and up to three pylons, fixed stores . Stores with up to two finned sections, vortical wing-tail interference, specified ejection forces, specified thrust/time history. Based on panel methods with simulation of nonlinear shock effects in flow field.
These codes run fast on workstations, reduce the need to conduct costly wind tunnel tests, and are indispensible in prelimanary safe store launch assessments and parent aircraft/store integration studies.
Marnix Dillenius
President
Nielsen Engineering & Research, Inc.
526 Clyde Avenue
Mountain View, CA 94043-2212
USA
415-968-9457
415-968-1410 (fax)
mfed@nearinc.com
For applications in related solution areas, see the following indices: Aerodynamics, Aerospace, Analysis, Simulation, the developer index for Nielsen Engineering & Research, Inc. and the market segment index for Computational Fluid Dynamics (CFD).
