NDLI: Body weight of hypersonic aircraft, part 1

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Body weight of hypersonic aircraft, part 1

Content Provider	NASA Technical Reports Server (NTRS)
Author	Ardema, Mark D.
Copyright Year	1988
Description	The load bearing body weight of wing-body and all-body hypersonic aircraft is estimated for a wide variety of structural materials and geometries. Variations of weight with key design and configuration parameters are presented and discussed. Both hot and cool structure approaches are considered in isotropic, organic composite, and metal matrix composite materials; structural shells are sandwich or skin-stringer. Conformal and pillow-tank designs are investigated for the all-body shape. The results identify the most promising hypersonic aircraft body structure design approaches and their weight trends. Geometric definition of vehicle shapes and structural analysis methods are presented in appendices.
File Size	1926757
Page Count	62
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19910000736
Archival Resource Key	ark:/13960/t3421vt7d
Language	English
Publisher Date	1988-10-01
Access Restriction	Open
Subject Keyword	Aircraft Design, Testing And Performance Structural Weight Composite Materials Aerodynamic Configurations Body-wing Configurations Aircraft Construction Materials Aircraft Design Composite Structures Design Analysis Hypersonic Aircraft Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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