NASA NTRS · 19720055957
Panel-flutter analysis of a thermal protection-shield concept for the space shuttle.
Abstract
Analysis of the panel flutter characteristics of a candidate thermal protection system (TPS) for the space shuttle, using piston theory aerodynamics and Lagrange equations. The results show the TPS candidate panel array to be deep in the 'no-flutter' region during launch and, therefore, safe from panel flutter.
Keep this discovery
Explore connections, maps & timelines
Cunningham, H. J.. 1972-08-01. Panel-flutter analysis of a thermal protection-shield concept for the space shuttle.. https://ntrs.nasa.gov/citations/19720055957
Cite the original work for its findings. Save a collection to share your selection of sources.