Development and Evaluation of Sensor Concepts for Ageless Aerospace Vehicles: Threats and Measurands
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Published: 2002
Total Pages: 28
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Published: 2002
Total Pages: 28
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Published: 2002
Total Pages: 140
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DOWNLOAD EBOOKAuthor: Pierre Gilles de Gennes
Publisher: Cambridge University Press
Published: 1997-04-28
Total Pages: 129
ISBN-13: 0521564174
DOWNLOAD EBOOKAn impressionistic tour of the physics of soft interfaces by Nobel Laureate Pierre Gilles de Gennes.
Author: S. Trickey
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 458
ISBN-13: 1468424181
DOWNLOAD EBOOKThe second International Symposium on Quantum Fluids and Solids came to pass during 23-27 Jan. 1977 as the fourth and con cluding part of the seventeenth consecutive running of the Sanibel Symposium Series. With approximately 120 participants from eleven countries (including, for the first time, the USSR), we found it easy to obtain a selection of papers which was fairly comprehen sive. Indeed, our problem was an embarrassment of riches; in spite of our solemn vows not to crowd the schedule, we ended up with an intense program! By far, the majority of the papers pre sented are represented in this volume. We are indebted to many persons and organizations for their contributions to the Symposia. First, we thank Prof. Per-Olov Lowdin, Director of the Quantum Theory Project and originator of the Sanibel Symposia. Without his patient, indulgent cooperation our task would have been vastly more difficult. We are grateful to Prof. F. Eugene Dunnam, Chairman of the Dept. of Physics and Astronomy, for providing Departmental support of our initial or ganlzlng expenses. Approximately one-half of the total cost of the Symposium was borne by a joint grant from the National Science Foundation and the U. S. Air Force Office of Scientific Research. We thank the program officers, Dr. C. Satterthwaite and Dr. D.
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Published: 1999
Total Pages: 46
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DOWNLOAD EBOOKBetween 1997 and 1999, a Working Group on the feasibility of collaborative, multi-facility windtunnel testing for the validation of Computational Fluid Dynamics Codes (CFD) has established the following results: Wintunnel tests are the main source of CFD validation but all have specific bias errors. Testing of the same model in several facilities can better establish the level of uncertainty in windtunnel tests and hence help assess possible differences between CFD and windtunnel tests. The Working Group, after an initial inquiry, established the need for CFD validation for fighter aircraft, transport type aircraft, missiles and helicopters. Effort and cost can be controlled efficiently and would permit the improvement of CFD Codes for considerable cost saving in future developments.
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Published: 1999
Total Pages: 486
ISBN-13:
DOWNLOAD EBOOKThe symposium dealt with design approaches for military aircraft propulsion systems to provide enhanced operational flexibility, longer range, better fuel efficiency and improved affordability. All classes of gas turbines were addressed in nine sessions as follows: Engine Design and Analysis (Part 1) (5 papers); Mechanical Systems (6 papers); Controls (4 papers); Combustors/Augmentors (4 papers); Compressor Systems (Part I) (5 papers); Compressor Systems (Part II) (3 papers); Turbines (Part I) (5 papers); Turbines (Part II) (4 papers); Engine Design and Analysis (Part II) (4 papers) These proceedings also include a Technical Evaluation Report and a Keynote address published in French and English.
Author: Workshop on Fatigue in the Presence of Corrosion
Publisher:
Published: 1999
Total Pages: 230
ISBN-13:
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Published: 1979
Total Pages: 236
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DOWNLOAD EBOOKAuthor: North Atlantic Treaty Organization. Research and Technology Organization
Publisher:
Published: 1998
Total Pages: 342
ISBN-13:
DOWNLOAD EBOOKContains the lecture notes prepared for a Special Course on Fluid Dynamics Research on Supersonic Aircraft organized by the RTO Applied Vehicle Technology Panel (AVT). The Course was held at the von Kármán Institute for Fluid Dynamics (VKI) Institute, Rhode-Saint-Genèse, Belgium 25-29 May 1998. The following topics were covered: History & Economics of Supersonic Transports, Supersonic Aerodynamics, Sonic Boom Theory and Minimization, Multi-Point Design Challenges, Vortex Plume Interactions, Propulsion System Design. Presentations on the major world wide supersonic transport programs were also included. The material assembled in this publication was prepared under the combined sponsorship of the RTO Applied Vehicle Technology Panel, the Consultant and Exchange Program of RTO, and the von Kármán Institute (VKI) for Fluid Dynamics.
Author: George C. Ashby
Publisher:
Published: 1965
Total Pages: 82
ISBN-13:
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