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Aerodynamic characteristics of a large scale model with a swept wing and augmented jet flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Koenig, D. G. Falarski, M. D. |
| Copyright Year | 1971 |
| Description | Data of tests of a large-scale swept augmentor wing model in the 40- by 80-foot wind tunnel are presented. The data includes longitudinal characteristics with and without a horizontal tail as well as results of preliminary investigation of lateral-directional characteristics. The augmentor flap deflection was varied from 0 deg to 70.6 deg at isentropic jet thrust coefficients of 0 to 1.47. The tests were made at a Reynolds number from 2.43 to 4.1 times one million. |
| File Size | 19052612 |
| Page Count | 103 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720004252 |
| Archival Resource Key | ark:/13960/t55f3k92c |
| Language | English |
| Publisher Date | 1971-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Configurations Swept Wings Aerodynamic Coefficients Wind Tunnel Models Aerodynamic Characteristics Aircraft Structures Sweptback Tail Surfaces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
