The paper reviews the results of some of the real-gas studies made at Langley that are directly related to establishing the range of operating conditions that can be used in a cryogenic nitrogen wind tunnel and still be assured of valid full-scale simulation. Consideration is given to the important aerodynamic features, anticipated performance capability, status of construction, and projected operating data for the National Transonic Facility.
Full scale aircraft simulation with cryogenic tunnels and status of the National Transonic Facility
International Symposium on Cryogenic Wind Tunnels ; 1979 ; Southampton
1979-01-01
Sonstige
Keine Angabe
Englisch
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