Proceedings of Symposium on Aeroelastic & Dynamic Modeling Technology
Report Number: RTD TDR 63-4197 Part I
Corporate Author(s): Research & Technology Division
Laboratory: Research & Technology Division
Date of Publication: 1964-03
Pages: 776
DoD Task:
Identifier: AD0434797
Abstract:
The unclassified proceedings of the Air Force Flight Dynamics Laboratory and Aerospace Industries Association Symposium on Aeroelastic and Dynamic Modeling Technology are presented in this report. Modern day aerospacecraft requirements are calling more and more for systems which are greatly influenced by aero and thermoelastic effects. In line with this trend, model testing technology has been required to keep pace by advancing the state-of-the-art in the simulation of elastic, thermal, aerodynamic and dynamic effects. The objective of this symposium was to bring together the members of the scientific community who are intimately concerned with this area of endeavor, thereby promoting a mutual understandinig of current developments and problem areas. The papers presented at the symposium were divided into appropriate technical area sub-groups and individual sessions were devoted to each. These sub-groups were: Theory and Design, Model Testing Techniques, Dynamic Loads and Aeroelastic Applications, and Structural Design Applications with two classified sessions on Aerospace Vehicle Applications and Aircraft Applications.
Provenance: Bombardier/Aero
Corporate Author(s): Research & Technology Division
Laboratory: Research & Technology Division
Date of Publication: 1964-03
Pages: 776
DoD Task:
Identifier: AD0434797
Abstract:
The unclassified proceedings of the Air Force Flight Dynamics Laboratory and Aerospace Industries Association Symposium on Aeroelastic and Dynamic Modeling Technology are presented in this report. Modern day aerospacecraft requirements are calling more and more for systems which are greatly influenced by aero and thermoelastic effects. In line with this trend, model testing technology has been required to keep pace by advancing the state-of-the-art in the simulation of elastic, thermal, aerodynamic and dynamic effects. The objective of this symposium was to bring together the members of the scientific community who are intimately concerned with this area of endeavor, thereby promoting a mutual understandinig of current developments and problem areas. The papers presented at the symposium were divided into appropriate technical area sub-groups and individual sessions were devoted to each. These sub-groups were: Theory and Design, Model Testing Techniques, Dynamic Loads and Aeroelastic Applications, and Structural Design Applications with two classified sessions on Aerospace Vehicle Applications and Aircraft Applications.
Provenance: Bombardier/Aero
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This conference contains the following reports:
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Front Matter RTD-TDR-63-4197 Part I, p. i-viii
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Opening Remarks RTD-TDR-63-4197 Part I, p. 1
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Welcome Address RTD-TDR-63-4197 Part I, p. 3
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Keynote Address RTD-TDR-63-4197 Part I, p. 5
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Opening Remarks of Session I RTD-TDR 63-4197 Part I, p. 11
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Dynamic Modeling - Its Past and Future RTD-TDR-63-4197 Part I, p. 13
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Analysis of Similitude Requirements and Scaling Laws for Transonic Buffeting RTD-TDR 63-4197 Part I, p. 49
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Dynamic Structural Modeling Using Dissimilar Materials RTD-TDR-63-4197 Part I, p. 81
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A Study of Thermal Scale Modeling Techniques RTD-TDR-63-4197 Part 1, p. 97
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Application of Aeroelastic Modeling Techniques to the Determination of Strctural Loads and Stability and Control Dynamic Characteristics RTD-TDR-63-4197 Part I, p. 129
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Dynamic Testing Techniques for a Wind Tunnel Model RTD-TDR-63-4197 Part I, p. 159
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A New "Free-flight" Mount System for High Speed Wind-Tunnel Flutter Models RTD-TDR-63-4197 Part I, p. 169
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Construction and Testing Techniques of Inflatable Flutter Models RTD-TDR-63-4197 Part I, p. 207
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Support Systems and Excitation Techniques for Dynamic Models of Space Vehicle Structures RTD-TDR-63-4197 Part I, p. 249
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Diagnosis of Flutter Model Response Using Time Correlation Techniques RTD-TDR-63-4197 Part I, p. 279
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Computer vs Model RTD-TDR-63-4197 Part I, p. 301
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On the Use of Dynamic Models for Studying Launch Vehicle Buffet and Ground-wind Loads RTD-TDR 63-4197 Part I, p. 333
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Simulation of Orbital Mooring of Gemini and Agena Vehicles by Means of Dynamically Scaled Models RTD-TDR-63-4197 Part I, p. 389
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Dynamic Modeling of Fuel Slosh RTD-TDR-63-4197 Part I, p. 417
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Development of Dynamic Model Rotor Blades for High Speed Helicopter Research RTD-TDR-63-4197 Part I, p. 431
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Dynamic Models for Low Cycle Fatigue RTD-TDR-63-4197 Part I, p. 511
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Haystack Antenna 1/15 Scale Model Program RTD-TDR-63-4197 Part I, p. 551
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Scientific Modelling for Photomechanics RTD-TDR-63-4197 Part I, p. 573
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The Use of Models for Control of Sonically Induced Vibration RTD-TDR-63-4197 Part I, p. 609
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Vibration Testing During High Heat Rates RTD-TDR-63-4197 Part I, p. 649
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Implications of Practical Re-entry Structures for Dynamic Model Simulation RTD-TDR 63-4197 Part I, p. 673
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Design and Construction Considerations of a Transonic-Supersonic Aeroelastic Flutter Model of X-20A RTD-TDR 63-4197 Part I, p. 703
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Dynamic Model Testing of the XC-142A Aircraft RTD-TDR-63-4197 Part I, p. 723
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Airframe Structural Testing - "Where Do We Go From Full Scale?" RTD-TDR-63-4197 Part I, p. 763
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Closing Remarks RTD-TDR-63-4197 Part I, p. 775