Compressive Strength Of 24s T Aluminum Alloy Flat Panels With Longitudinal Formed Hat Section Stiffeners Having A Ratio Of Stiffener Thickness To Skin Thickness Equal To 100
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Author | : William A. Hickman |
Publisher | : |
Total Pages | : 558 |
Release | : 1947 |
Genre | : Aluminum alloys |
ISBN | : |
Results are present for part of a test program on 24S-T aluminum-alloy flat compression panels with hat-section stiffeners. The results show the effect of the relative dimensions of a panel on the buckling stress and average stress at maximum load. Comparative envelope curves are presented to provide some indication of the relative structural efficiencies of hat- and Z-stiffened panels having a ratio of stiffener thicknews to skin thickness of one.
Author | : Society of Automotive Engineers |
Publisher | : |
Total Pages | : 1316 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : Society of Automotive Engineers |
Publisher | : |
Total Pages | : 710 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : New York Public Library. Economic and Public Affairs Division |
Publisher | : |
Total Pages | : 794 |
Release | : 1972 |
Genre | : Government publications |
ISBN | : |
Author | : Thomas Henry Gordon Megson |
Publisher | : Hodder Education |
Total Pages | : 0 |
Release | : 1990 |
Genre | : Aeroelasticity |
ISBN | : 9780713136814 |
This book provides a self-contained course in aircraft structures which contains not only the fundamentals of elasticity and aircraft structural analysis but also the associated topics of airworthiness and aeroelasticity.
Author | : Joseph R. Davis |
Publisher | : ASM International |
Total Pages | : 338 |
Release | : 1999-01-01 |
Genre | : Technology & Engineering |
ISBN | : 9781615032389 |
Author | : Ronald D. Ziemian |
Publisher | : John Wiley & Sons |
Total Pages | : 1120 |
Release | : 2010-02-08 |
Genre | : Technology & Engineering |
ISBN | : 0470085258 |
The definitive guide to stability design criteria, fully updated and incorporating current research Representing nearly fifty years of cooperation between Wiley and the Structural Stability Research Council, the Guide to Stability Design Criteria for Metal Structures is often described as an invaluable reference for practicing structural engineers and researchers. For generations of engineers and architects, the Guide has served as the definitive work on designing steel and aluminum structures for stability. Under the editorship of Ronald Ziemian and written by SSRC task group members who are leading experts in structural stability theory and research, this Sixth Edition brings this foundational work in line with current practice and research. The Sixth Edition incorporates a decade of progress in the field since the previous edition, with new features including: Updated chapters on beams, beam-columns, bracing, plates, box girders, and curved girders. Significantly revised chapters on columns, plates, composite columns and structural systems, frame stability, and arches Fully rewritten chapters on thin-walled (cold-formed) metal structural members, stability under seismic loading, and stability analysis by finite element methods State-of-the-art coverage of many topics such as shear walls, concrete filled tubes, direct strength member design method, behavior of arches, direct analysis method, structural integrity and disproportionate collapse resistance, and inelastic seismic performance and design recommendations for various moment-resistant and braced steel frames Complete with over 350 illustrations, plus references and technical memoranda, the Guide to Stability Design Criteria for Metal Structures, Sixth Edition offers detailed guidance and background on design specifications, codes, and standards worldwide.
Author | : John Dwight |
Publisher | : CRC Press |
Total Pages | : 314 |
Release | : 1998-12-10 |
Genre | : Architecture |
ISBN | : 1135831769 |
Provides a practical design guide to the structural use of aluminium. The first chapters outline basic aluminium technology and the advantages of using aluminium in many structural applications. The major part of the book deals with structural design and presents very clear guidance for designers, with numerous diagrams, charts and examples.
Author | : Edward M. Lenoe |
Publisher | : Springer Science & Business Media |
Total Pages | : 858 |
Release | : 2012-12-06 |
Genre | : Technology & Engineering |
ISBN | : 1468410334 |
The Fourth Conference on Fibrous Composites in Structural Design was a successor to the First-to-Third Conferences on Fibrous Composites in Flight Vehicle Design sponsored by the Air Force (First and Second Conferences, September 1973 and May 1974) and by NASA (Third Conference, November 1975) which were aimed at focusing national attention on flight vehicle applications of a new class of fiber reinforced materials, the advanced com posites, which afforded weight savings and other advantages which had not been previously available. The Fourth Conference, held at San Diego, California, 14-17 November 1978, was the fi rst of these conferences to be jointly sponsored by the Army, Navy and Ai r Force together with NASA, as well as being the first to give attention to non-aerospace applications of fiber reinforced composites. While the design technology for aerospace applications has reached a state of relative maturity, other areas of application such as mi litary bridging, flywheel energy storage systems, ship and surface vessel components and ground vehicle components are in an early stage of development, and it was an important objective to pinpoint where careful attention to structural design was needed in such applications to achfeve maximum structural performance payoff together with a high level of reliability and attractive economics.
Author | : Peter W. Merlin |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 240 |
Release | : 2008 |
Genre | : History |
ISBN | : |
The Lockheed Blackbirds hold a unique place in the development of aeronautics. In their day, the A-12, YF-12, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. Now retired, they remain the only production aircraft capable of sustained Mach 3 cruise and operational altitudes above 80,000 feet.This is the first book to address the technical aspects of these incredible aircraft. The author describes the design evolution of the Blackbird, from the Archangel to the Senior Crown (the Air Force's SR-71.) He describes in detail the construction and materials challenges faced by Lockheed, as well as the Blackbird's performance characteristics and capabilities.A NASA historian, the author describes NASA's role in using the aircraft as a flying laboratory to collect data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft. The reader will benefit from the technical and programmatic lessons learned.This volume was produced in cooperation with the National Aeronautics and Space Administration.