Application of Multivariable Search Techniques to the Shaping of Minimum Total Heat Reentry Bodies at Hyperbolic Velocity PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Application of Multivariable Search Techniques to the Shaping of Minimum Total Heat Reentry Bodies at Hyperbolic Velocity PDF full book. Access full book title Application of Multivariable Search Techniques to the Shaping of Minimum Total Heat Reentry Bodies at Hyperbolic Velocity by Donald S. Hague. Download full books in PDF and EPUB format.
Author: Donald S. Hague
Publisher:
ISBN:
Category :
Languages : en
Pages : 146
Get Book Here
Book Description
Author: Donald S. Hague
Publisher:
ISBN:
Category :
Languages : en
Pages : 146
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 160
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 344
Get Book Here
Book Description
Author: D. S. Hague
Publisher:
ISBN:
Category : Mathematical optimization
Languages : en
Pages : 172
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Electronic data processing
Languages : en
Pages : 492
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 862
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 366
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1124
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Computer science
Languages : en
Pages : 482
Get Book Here
Book Description
Author: Brent Silver
Publisher:
ISBN:
Category : Structural design
Languages : en
Pages : 62
Get Book Here
Book Description
The application of optimization techniques to aircraft configuration design is discussed. Advantages and disadvantages of automated search methods are compared with those of parametric analysis methods. The formulation of the design problem for direct search methods using a normalization procedure is developed. Various direct methods are briefly described. Operational results using several of these methods are reported for aircraft configuration design problems. Gradient methods are found to give disappointing results when compared with certain non-gradient methods. Reasons are suggested for this behavior. The future promise of 'man-computer interactive design' is briefly described. (Author).
