Optimization under aeroelastic constraintsOptimization of aeroelastic constraints for aircraft design using differential equation idealization and finite element approximation
Document ID
19710010664
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ashley, H. (Advisory Group for Aerospace Research and Development Paris, France)
Mc Intosh, S. C., Jr. (Advisory Group for Aerospace Research and Development Paris, France)
Weatherill, W. H. (Advisory Group for Aerospace Research and Development Paris, France)
Date Acquired
August 6, 2013
Publication Date
February 1, 1971
Publication Information
Publication: STRUCTURAL DESIGN APPL. OF MATHEMATICAL PROGRAMMING TECH. FEB. 1971