Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow [PDF]
Chinese Journal of Aeronautics, 2018 Analytical indicial aerodynamic functions are calculated for several trapezoidal wings in subsonic flow, with a Mach number 0.3≤ Ma≤ 0.7. The formulation herein proposed extends well-known aerodynamic theories, which are limited to thin aerofoils in incompressible flow, to generic trapezoidal wing planforms.
Da Ronch, Andrea +5 more
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2001 An experimental study on the improvement of aerodynamic characteristics of a modified arrow wing by applying lateral blowing in subsonic flow has been conducted. The modified arrow wing, which is one of the baseline configurations of the proto-type of next-generation SST, is selected for the experiments.
Kiyoshi Sato +3 more
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SUSSA ACTS: A computer program for steady and unsteady, subsonic and supersonic aerodynamics for aerospace complex transportation systems [PDF]
The computer program SUSSA ACTS (Steady and Unsteady, Subsonic and Supersonic Aerodynamics for Complex Transportation Systems) are presented in the final version.
Morino, L., Tseng, K.
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The finite element method in low speed aerodynamics [PDF]
The finite element procedure is shown to be of significant impact in design of the 'computational wind tunnel' for low speed aerodynamics. The uniformity of the mathematical differential equation description, for viscous and/or inviscid, multi ...
Baker, A. J., Manhardt, P. D.
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Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design [PDF]
Progress in the development of computational methods for steady and unsteady aerodynamics has perennially paced advancements in aeroelastic analysis and design capabilities. Since these capabilities are of growing importance in the analysis and design of
Yates, E. Carson, Jr.
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Fully unsteady subsonic and supersonic potential aerodynamics for complex aircraft configurations for flutter applications [PDF]
A general theory for study, oscillatory or fully unsteady potential compressible aerodynamics around complex configurations is presented. Using the finite-element method to discretize the space problem, one obtains a set of differential-delay equations ...
Morino, L., Tseng, K.
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A survey of computational aerodynamics in the United States [PDF]
Programs in theoretical and computational aerodynamics in the United States are described. Those aspects of programs that relate to aeronautics are detailed.
Gessow, A., Morris, D. J.
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Overview of the Applied Aerodynamics Division [PDF]
A major reorganization of the Aeronautics Directorate of the Langley Research Center occurred in early 1989. As a result of this reorganization, the scope of research in the Applied Aeronautics Division is now quite different than that in the past.
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Subsonic flutter analysis addition to NASTRAN [PDF]
, 1973 A subsonic flutter analysis capability has been developed for NASTRAN, and a developmental version of the program has been installed on the CDC 6000 series digital computers at the Langley Research Center.
Doggett, R. V., Jr., Harder, R. L.
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Aeronautical Engineering: A special bibliography with indexes, supplement 67, February 1976 [PDF]
This bibliography lists 341 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...
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