原文传递
User manual for NASA Lewis 10 by 10 foot supersonic wind tunnel
| 题名： | User manual for NASA Lewis 10 by 10 foot supersonic wind tunnel |
| 作者： | Soeder, Ronald H. |
| 关键词： | supersonic；tunnel；lewis；manual；nasa；user；pressure；temperature；processing；section |
| 摘要： | This manual describes the 10- by 10-Foot Supersonic Wind Tunnel at the NASA Lewis Research Center and provides information for users who wish to conduct experiments in this facility. Tunnel performance operating envelopes of altitude, dynamic pressure, Reynolds number, total pressure, and total temperature as a function of test section Mach number are presented. Operating envelopes are shown for both the aerodynamic (closed) cycle and the propulsion (open) cycle. The tunnel test section Mach number range is 2.0 to 3.5. General support systems, such as air systems, hydraulic system, hydrogen system, fuel system, and Schlieren system, are described. Instrumentation and data processing and acquisition systems are also described. Pretest meeting formats and schedules are outlined. Tunnel user responsibility and personnel safety are also discussed. |
| 报告类型： | 科技报告 |
相关文献
- Subsonic Flow Quality Surveys of the NASA Lewis Research Center 10- by 10-Foot Supersonic Wind Tunnel
- Low-Pressure Capability of NASA Glenn's 10- by 10-Foot Supersonic Wind Tunnel Expanded
- Calibration of the NASA Glenn Research Center 10-by 10-ft Supersonic Wind Tunnel (1993 and 1995 Tests)
- Baseline Calibration of the NASA Lewis Research Center 8-by 6-Foot Supersonic Wind Tunnel (1991 and 1992 Tests)
- New Test Section Installed in NASA Lewis' 1- by 1-Foot Supersonic Wind Tunnel
- Flow Field Surveys of the NASA Lewis Research Center 8- by 6-Foot Supersonic Wind Tunnel (1993 Test)
检索历史
应用推荐
