Advanced hypersonic test facilities
著者
書誌事項
Advanced hypersonic test facilities
（Progress in astronautics and aeronautics, v. 198）
American Institute of Aeronautics and Astronautics, c2002
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内容説明・目次
内容説明
This volume on hypersonic test facilities covers such topics as: requirements; principles of test facility development; NASA's HYPULSE facility at GASL; the LENS I and II hypervelocity tunnels; the U-12 large shock tube; and detonation-driven shock tubes and tunnels.
目次
- Hypersonic Ground Test Requirements
- Principles of Hypersonic Test Facility Development
- NASA's HYPULSE Facility at GASL
- The LENS I and II Hypervelocity Tunnels and Application to Hypersonic Vehicle Testing Under Fully Duplicated Flight Conditions
- The U-12 Large Shock Tube
- Detonation-Driven Shock Tubes and Tunnels
- Aerothermodynamics Research in the DLR High Enthalpy Shock Tunnel HEG
- Characteristics of the HIEST and its Applicability for Hypersonic Aerothermodynamic and Scramjet Research
- Piston Gasdynamic Units with Multicascade Compression
- Arc-Heated Facilities
- The SCIROCCO 70-MW Plasma Wind Tunnel
- Aerodynamic and Propulsion Test Unit
- Arc-Heated Facilities (LBK) as a Tool to Study Aerothermodynamic Problems of Reentry Vehicles
- The NASA Langley Research Center 8-ft High Temperature Tunnel
- NASA Glenn Research Center's Hypersonic Tunnel Facility
- The ONERA F4 High-Enthalpy Wind Tunnel
- The AEDC Hypervelocity Wind Tunnel 9
- A Hypersonic Ground-Test Facility Using Magnetic Levitation and Electromagnetic Propulsion
- Recent Increases in Hypersonic Test Capabilities at the Holloman High Speed Test Track and Design of a Magnetically Levitated Test Track Capability
- Increased Launching Capabilities at AEDC's Range/Track G
- A New Mach 8-15 True Temperature Test Facility Concept to Meet the U.S. Shortfall in Hypersonic Test Capability
- New-Generation Hypersonic Adiabatic Compression Facilities with Pressure Multipliers
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