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Report of the panel on dynamics and aeroelasticity. [transonic tunnel capabilities
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Houbolt, J. |
| Copyright Year | 1977 |
| Description | Model scaling for flutter analysis is reviewed. Characteristics of the Langley Transonic Dynamics Tunnel (TDT) are described and several features are recommended for inclusion in the National Transonic Facility. Problem areas suggested for the NTF include: Reynolds number effects on control surface unsteady aerodynamics; effects of Reynolds number on buffet onset and loads; transonic unsteady aerodynamics; and Reynolds number effects on flutter characteristics of wing planforms and airfoils. |
| File Size | 1432536 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770020206 |
| Archival Resource Key | ark:/13960/t55f3md5k |
| Language | English |
| Publisher Date | 1977-01-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Dynamic Characteristics Temperature Effects Transonic Wind Tunnels Unsteady Aerodynamics Inertia Wind Tunnel Models Flutter Analysis Aerodynamic Stability Aeroelasticity Aircraft Structures Aerodynamic Loads Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |