Supersonic Aeroelastic Effects on Static Stability and Control: Aeroelastic interaction, by V. W. Donato
Author: Bell Aircraft Corporation
Publisher:
Published: 1958
Total Pages: 374
ISBN-13:
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Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aerodynamics
Thermoelastic Effects on Hypersonic Stability and Control: Hypersonic aeroelasticity
Thermal Effects on Static Aeroelastic Stability and Control: sup. Description and results of tests conducted to determine the thermally affected behavior of corrugated multiweb wing structures, by J. F. Quinn
Proceedings of Symposium on Aerothermoelasticity
Author: David M. Jones
Publisher:
Published: 1962
Total Pages: 1028
ISBN-13:
DOWNLOAD EBOOK →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.
Nonlinear Thermoelastic Effects on Hypersonic Stability and Control
ASD Technical Report
International Aerospace Abstracts
A Measurement of the Static Aeroelastic Deformation and Loading of a Wing in Supersonic Flow
Author: Frank Herman Durgin
Publisher:
Published: 1963
Total Pages: 90
ISBN-13:
DOWNLOAD EBOOK →The aeroelastic analysis of Zisfein, Donato and Farrell (AD-155739) uses an aerodynamic matrix, a structural matrix and the initial angle of attack to predict the equilibrium pressures and shape of a wing. To test the accuracy of their methods, a flexible wing was built and instrumented with pressure taps and mirrors. The wing was tested at Mach numbers of 2 and 3, and both the pressure distribution and the deflected shape were measured. An aerodynamic matrix computed on the basis of the semiempirical procedures of the above authors was used to predict pressure distributions, and an experimentally determined structural matrix was used to find equilibrium angles of attack. Finally, these two matrices were used in the aeroelastic equations to compute pressures and angles of attack from the undeflected shape of the wing. Comparisons between theory and experiment are presented for eight different free stream conditions. -- page iii.
Introduction to Aircraft Aeroelasticity and Loads
Author: Jan Robert Wright
Publisher: John Wiley & Sons
Published: 2008-02-28
Total Pages: 559
ISBN-13: 047085846X
DOWNLOAD EBOOK →Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.
