HiMAP: a portable super modular multilevel parallel multidisciplinary process for large scale analysis

Author:

Guruswamy G.P

Publisher

Elsevier BV

Subject

General Engineering,Software

Reference16 articles.

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2. Slotnick JP, Kandula M, Buning PG. Navier–Stokes simulation of the space shuttle launch vehicle flight transonic flowfield using a large scale Chimera grid system. AIAA-94-1860.

3. ENSAERO—a multidisciplinary program for fluid/structural interaction studies of aerospace vehicles;Guruswamy;Computing Systems Engng,1990

4. Schuster D, Vadyak J, Atta E. Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier–Stokes algorithm. AIAA Paper 90-0435, 1990.

5. Development of aeroelastic capability;Gupta;J Aircraft,1996

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2. Large-Scale Computations for Stability Analysis of Launch Vehicles Using Cluster Computers;Journal of Spacecraft and Rockets;2011-07

3. High Fidelity Dynamic Analysis of Launch Vehicles on Single-Image Supercomputers;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18

4. Study on the Use of High-Fidelity Methods in Aeroelastic Optimization;Journal of Aircraft;2004-05

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