Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers-Reference-Cited by-同舟云学术

Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
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Author:

Reuther J.¹,Jameson A.²,Alonso J.²,Rimlinger M.¹,Sauders D.¹,Reuther J.¹,Jameson A.²,Alonso J.²,Rimlinger M.¹,Sauders D.¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

2. Princeton Univ., NJ

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-103

Reference38 articles.

1. P.E. GUI,W.Murray,M.A.Saunders,andM.A.Wright. User's guideforNPSOL (version 4.0).aFORTRANpackagenonlinear programming. Technical Report SOL86-2, Stanford University,DepartmentofOperationsResearch,1986.

2. P.E.Gill,W.Murray,andM.H.Wright.PracticalOptimization. AcademicPress,1981.

3. Wing Design by Numerical Optimization

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