Design Features and Operational Characteristics of the Langley Pilot Transonic Cryogenic Tunnel
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CENTER
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A theoretical investigation by Smelt in 1945 indicated that the use of air at cryogenic temperatures would permit larged reductions of wind-tunnel size and power requirements in comparision with a wind tunnel operated at normal tmeperature.
- Test Facilities, Equipment and Methods
- Fluid Mechanics