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A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390
| Content Provider | University of North Texas |
|---|---|
| Author | Bielat, Ralph P. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation of the aerodynamic characteristics of a model of the Grumman F9F-9 airplane in the transonic tunnel. Results regarding the transonic drag-rise increment, drag analysis, and effective downwash angle are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc53143 |
| Language | English |
| Publisher Date | 2019-01-22 |
| Access Restriction | Open |
| Subject Keyword | Grumman F9F-9 aerodynamics drag coefficients |
| Content Type | Text |
| Resource Type | Report |