Proceedings of Symposium on Aerothermoelasticity
Proceedings of Symposium on Aerothermoelasticity

Author: David M. Jones

Publisher:

Published: 1962

Total Pages: 1028

ISBN-13:

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A symposium on Aerothermoelasticity was held to present the latest significant developments in each scientific area and engineering area that comprise the component parts of this technology. New and significant contributions were presented in four technical areas consisting of dynamic aerothermoelasticity (flutter), stability and control, thermodynamics and aerodynamics (or aerothermodynamics), and structures including material and construction concepts. Categories important and significant to each technical area are discussed state-of-the-art wise. In addition, 26 separate papers are given on items of special importance.

Theory of Matrix Structural Analysis
Theory of Matrix Structural Analysis

Author: J. S. Przemieniecki

Publisher: Courier Corporation

Published: 1985-01-01

Total Pages: 502

ISBN-13: 9780486649481

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This classic text begins with an overview of matrix methods and their application to the structural design of modern aircraft and aerospace vehicles. Subsequent chapters cover basic equations of elasticity, energy theorems, structural idealization, a comparison of force and displacement methods, analysis of substructures, structural synthesis, nonlinear structural analysis, and other topics. 1968 edition.

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Iii: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Iii: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing

Author: James R. BATT

Publisher:

Published: 1965

Total Pages: 57

ISBN-13:

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Results are presented of additional nonlinear structuralaerodynamic interaction experiments and analyses conducted on a 45 degree delta wing. The aeroelastic simulation scheme developed and described in AD-608 476 was used to experimentally determine the static aerothermoelastic behavior of the subject model wing. Test data were compared with theoretical predictions using a digital computer program. (Author).

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Ii. Analytical and Experimental Static Aerothermoelasticity
Nonlinear Thermoelastic Effects on Hypersonic Stability and Control. Part Ii. Analytical and Experimental Static Aerothermoelasticity

Author: James R. Batt

Publisher:

Published: 1964

Total Pages: 90

ISBN-13:

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An analytical method was developed for the analysis of static aerothermoelastic behavior in the presence of nonlinear aerodynamic loads and geometrically nonlinear structural behavior. The method was programmed for the IBM 7090 digital computer using FORTRAN coding techniques. A system for the experimental determination of static aerothermoelastic response of nonuniformly heated structures to loadings which are a nonlinear function of wing surface slopes was developed. Results of this experimental program are presented and compared with theoretical predictions. (Author).