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Aircraft Design Digital Library
Volume 1. Structures, Materials, and Fasteners
The Aircraft Design Digital Library is a series of
CD-ROMs containing collections of reports and documents on various subjects
relating to aircraft design. This series is an essential addition to any
professional or amateur aircraft designer's library and provides immediate
access to essential design data and information.
The first volume in this series, Structures,
Materials, and Fasteners, covers the structural aspects of aircraft
design. This CD-ROM includes over 150 technical reports and documents that
provide information on aircraft structural design, aerospace material
properties, and appropriate methods for fastening or joining various structural
materials. Included in the collection are comprehensive material
properties data on the vast majority of all metal alloys, composite materials,
and wood varieties. These reports have been gathered from NASA, NACA (the
predecessor to NASA, the National Advisory Committee for Aeronautics), and the US
Department of Defense.
Selected Contents
The table below includes a small selection from the
over 150 documents included on the CD. The CD includes well over 5,000
pages of information. Click on the document titles below to view an
abstract.
| Document Title |
Document Number |
| Metallic Materials and Elements for Aerospace Vehicle Structures
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MIL-HDBK-5H
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| Composite Materials Handbook, Volume 1., Polymer Matrix Composites, Guidelines
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MIL-HDBK-17B
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Composite Materials Handbook, Volume 2., Polymer Matrix Composites, Materials Properties |
MIL-HDBK-17-2E
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Composite Materials Handbook, Volume 3. Polymer Matrix Composites, Materials Usage, Design and Analysis |
MIL-HDBK-17-3E
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Composite Materials Handbook, Volume 4., Metal Matrix Composites |
MIL-HDBK-17-4
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PREPARATION FOR AND INSTALLATION OF RIVETS AND SCREWS, ROCKET, MISSILE, AND
AIRFRAME STRUCTURES |
MIL-STD-403C
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NASA Fastener Design Manual |
NASA-RP-1228
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Potential structural materials and design concepts for light aircraft
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NASA-CR-1285
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Seat design for crash worthiness |
NACA Report 1332
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Strength of welded aircraft joints |
NACA Report 584
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The design of plywood webs for airplane wing beams |
NACA Report 344
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The design of airplane wing ribs |
NACA Report 345
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Strength of welded joints in tubular members for aircraft |
NACA Report 348
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Aircraft woods- their properties, selection, and characteristics |
NACA Report 354
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Price
The Structures, Materials and
Fasteners CD-ROM is $45
and is available through our online store.
Availability
The current edition of the Structures, Materials and Fasteners CD-ROM is our
July 2006 release and it is available now.
Software Requirements
The CD-ROM is formatted for Windows-based systems, but
the contents are platform neutral. The CD-ROM can be used on any system
that can view HTML and Adobe PDF files. Windows 95/98/ME/NT 4/2000/XP/Vista are
all supported.
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