Wing-Body Aercelasticity Using Finite-Difference Fluid/Finite-Element Structural Equations on Parallel Computers

Wing-Body Aercelasticity Using Finite-Difference Fluid/Finite-Element Structural Equations on Parallel Computers

Author(s):

Byun, C. ( NASA Ames Research Center )
Guruswamy, G.P.

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19960021635

Issue:

NASA-TM-111450

Pt.:

NAS 1.15:111450

Paper no.:

N96-24942

Page(from):

1

Page(to):

16

Pages:

16

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001432

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