3 edition of Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel found in the catalog.
Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel
by NASA Ames Research Center, Dryden Flight Research Facility, National Technical Information Service, distributor] in Edwards, Calif, [Springfield, Va
Written in English
|Statement||Larry D. Hudson and Randolph C. Thompson.|
|Series||NASA technical memorandum -- 101733.|
|Contributions||Thompson, Randolph C., Dryden Flight Research Facility.|
|The Physical Object|
|Number of Pages||21|
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Get this from a library. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel.
[Larry D Hudson; Randolph C Thompson; Dryden Flight Research Facility.]. Single-Strain-Gage Force/Stiffness Buckling Prediction Techniques On A H at-Stiffened Panel Author: Larry D.
Hudson and Randolph C. Thompson Subject: NASA TM Keywords: Elevated temperatures; foil strain gages; force/stiffness; hat-stiffened panel; hypersonic vehicle; NASTRAN; overall panel buckling Created Date: 12/27/ PM. This chapter discusses the experimental methods for high-temperature aerospace structures.
It places the emphasis on airframe and spacecraft structures. The development of thermal structural test capabilities after World War II was strongly motivated by problems disclosed by the early supersonic : Earl A. Thornton. Critical Buckling Pressure in Mouse Carotid Arteries with Altered Elastic Fibers.
PubMed Central. Luetkemeyer, Callan M.; James, Rhys H.; Devarakonda, Siva Teja; Le. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel.
NASA Technical Reports Server (NTRS) Hudson, Larry D.; Thompson, Randolph C. Predicting the buckling characteristics of a test panel is necessary to ensure panel integrity during a test program.