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Aerodynamic results of support system interference effects tests conducted in nasa/arc 6 by 6-foot supersonic wind tunnel using an 0.015-scale model of the configuration 14oa/b ssv orbiter (oa59), volume 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Campbell II, J. H. Embury, W. R. |
| Copyright Year | 1974 |
| Description | An experimental aerodynamic investigation was conducted in the NASA/ARC 6- by 6-foot supersonic wind tunnel on an 0.015-scale configuration 140A/B SSV Orbiter model. The primary objective was to determine the extent aerodynamic simulation is compromised by sting base mounting with MPS nozzles removed. Both a conventional sting (through the base) and an alternate model mounting system were utilized. The alternate mounting system consisted of a non-metric blade strut, which approximated the vertical tail and entered the model through the upper aft section of its fuselage. The model was tested both in and out of the presence of a dummy sting with and without MPS nozzles when on the alternate mounting system. Data were obtained at Mach numbers from 0.6 through 2.0, a Reynolds number of 2.5 million per foot, angles of attack from -4 through 14 degrees, angles of sideslip from -15 through 15 degrees, elevon deflections of 0 and 15 degrees, and bodyflap deflections of -11.7, 0, and 16.3 degrees. |
| File Size | 40344257 |
| Page Count | 682 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750002036 |
| Archival Resource Key | ark:/13960/t1qg3gm3v |
| Language | English |
| Publisher Date | 1974-09-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Supports Subsonic Speed Supersonic Speed Supersonic Wind Tunnels Wind Tunnel Tests Transonic Speed Nozzles Wind Tunnel Models Aerodynamic Characteristics Space Shuttle Orbiters Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
