Aerodynamic Shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Parallel Computers

Aerodynamic Shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Parallel Computers

Author(s):

Reuther, James ( Research Inst. for Advanced Computer Science )
Alonso, Juan Jose ( Princeton Univ. )
Rimlinger, Mark J. ( NASA Ames Research Center )
Jameson, Antony ( Princeton Univ. )

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19970000805

Issue:

NASA-CR-202390

Pt.:

NAS 1.26:202390

Page(from):

1

Page(to):

24

Pages:

24

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001434

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