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3 edition of Development of direct-inverse 3-D methods for applied aerodynamic design and analysis found in the catalog.

Development of direct-inverse 3-D methods for applied aerodynamic design and analysis

Development of direct-inverse 3-D methods for applied aerodynamic design and analysis

semiannual progress report, July 1, 1987 - December 31, 1987

by

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  • 34 Currently reading

Published by Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, National Aeronautics and Space Administration, National Technical Information Service, distributor in College Station, Tex, [Washington, DC, Springfield, Va .
Written in English


Edition Notes

Other titlesDevelopment of direct inverse three D methods for applied aerodynamic design and analysis
StatementLeland A. Carlson
SeriesNASA contractor report -- NASA CR-182436, TAMRF report -- no. 5373-88-01
ContributionsUnited States. National Aeronautics and Space Administration
The Physical Object
FormatMicroform
Pagination1 v
ID Numbers
Open LibraryOL18004730M

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Development of direct-inverse 3-D methods for applied aerodynamic design and analysis Download PDF EPUB FB2

Get this from a library. Development of direct-inverse 3-D methods for applied aerodynamic design and analysis: semiannual progress report, July 1, - Decem [Leland A Carlson; United States. National Aeronautics and Space Administration.]. Get this from a library. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: semiannual progress report, January 1, - J [Leland A Carlson; United States.

National Aeronautics and Space Administration.]. A viscous inverse method for aerodynamic design. There are several kinds of inverse design methods with different flow calculation approaches and different choices of prescribed quantities. These authors applied the new MGM design method, also using FPE aerodynamic analysis codes as a basis, to airfoil, axisymmetric nacelle inlet, and 3-D nacelle inlet design problems.

Later, Hazarika'^ and Sankar used a FPE CFD method to apply the MGM procedure to the design of blended wing-body configurations. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis [microform]: semiannual progress report, January 1, - J [] Carlson, Leland A.

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Part I: 2-D and Quasi 3-D Theory and Application, AGARD-R Development of direct-inverse 3-D methods for applied aerodynamic design and analysis book Design Methods for Aerodynamics, –» Google Scholar [Dedoussis93] Dedoussis, V., Chaviaropouios, P., and Papailiou, K.D., (): Rotational Compressible Inverse Design Method for Two-Dimensional, Internal Flow Configurations, AIAA Jour No.

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Numerical and approximate methods for calculating aerodynamic characteristics of MaRVs. A direct-inverse transonic wing-design method in curvilinear. This work also includes design and analysis of two stage op-amp and folded cascade op-amp to give gain higher than 70 dB and tradeoffs among the parameters such as.

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The. The reason for the latter is that the airfoil aerodynamic quantities do not vary consistently enough when boundary layer and potential flow are coupled in the weak interaction sense.

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