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A unique facility for v/stol aircraft hover testing. [langley impact dynamics research facility
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Culpepper, R. G. Gillespie, E. A. Lane, A. G. Murphy, R. D. |
| Copyright Year | 1979 |
| Description | The Langley Impact Dynamics Research Facility (IDRF) was modified to obtain static force and moment data and to allow assessment of aircraft handling qualities during dynamic tethered hover flight. Test probe procedures were also established. Static lift and control measurements obtained are presented along with results of limited dynamic tethered hover flight. |
| File Size | 2895838 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790021028 |
| Archival Resource Key | ark:/13960/t2b902n3b |
| Language | English |
| Publisher Date | 1979-08-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Dynamic Response Flight Tests Flight Characteristics Anions Dynamic Tests V/stol Aircraft Research Facilities Tethering Ground Effect Aerodynamics Hovering Static Tests Aircraft Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |