ANALYSIS OF THE FLUTTER OF FLAT RECTANGULAR PANELS ON THE BASIS OF EXACT THREE-DIMENSIONAL LINEARIZED SUPERSONIC POTENTIAL FLOW
Overview & Synopsis
Analysis of flutter of flat rectangular panels at low supersonic mach numbers using air forces from exact linearized potential-flow theory
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
Document Information
| Document Title | ANALYSIS OF THE FLUTTER OF FLAT RECTANGULAR PANELS ON THE BASIS OF EXACT THREE-DIMENSIONAL LINEARIZED SUPERSONIC POTENTIAL FLOW |
|---|---|
| Author / Organization | Cunningham, H. J. |
| Subject & Discipline | PREPRINT |
| Categories | Aerospace & Aviation |
| Publication Year | 2019 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-73139 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |