Linked Data Explorerhttp://worldcat.org/entity/work/id/198794080
High-lift flight tunnel phase II report
The High-Lift Flight Tunnel (HiLiFT) concept is a revolutionary approach to aerodynamic ground testing. This concept utilizes magnetic, levitation and linear motors to propel an aerodynamic model through a tube containing a quiescent test medium. This medium (nitrogen) is cryogenic and pressurized to achieve full flight Reynolds numbers higher than any existing ground test facility world-wide for the range of 0.05 to 0.50 Mach. The results of the Phase II study provide excellent assurance that the HiLiFT concept will provide a valuable low-speed, high Reynolds number ground test facility. The design studies concluded that the HiLiFT facility is feasible to build and operate and the analytical studies revealed no insurmountable difficulties to realizing a practical high Reynolds number ground test facility.
Open All Close All
http://schema.org/about
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/high_reynolds_number
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/ground_tests
- http://id.loc.gov/authorities/subjects/sh85113557
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/test_facilities
- http://id.worldcat.org/fast/1148251
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/wind_tunnel_tests
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/mach_number
- http://id.worldcat.org/fast/1096833
- http://id.loc.gov/authorities/subjects/sh85146907
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/cryogenic_equipment
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/reynolds_number
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/lift
- http://id.loc.gov/authorities/subjects/sh85134151
- http://id.worldcat.org/fast/998431
- http://id.loc.gov/authorities/subjects/sh85076855
- http://experiment.worldcat.org/entity/work/data/198794080#Topic/flight_tests
- http://id.worldcat.org/fast/1004756
- http://id.loc.gov/authorities/subjects/sh85079305
- http://id.worldcat.org/fast/1175706
http://schema.org/contributor
- http://worldcat.org/entity/person/id/2628741957
- http://experiment.worldcat.org/entity/work/data/198794080#Organization/mse_technology_application_inc
- http://worldcat.org/entity/person/id/2667292879
- http://id.loc.gov/authorities/names/n78087581
- http://experiment.worldcat.org/entity/work/data/198794080#Organization/united_states_national_aeronautics_and_space_administration
- http://worldcat.org/entity/person/id/2640326757
- http://viaf.org/viaf/127305149
- http://experiment.worldcat.org/entity/work/data/198794080#Organization/langley_research_center
- http://viaf.org/viaf/146202023
- http://id.loc.gov/authorities/names/n79134855
- http://experiment.worldcat.org/entity/work/data/198794080#Organization/mse_technology_applications_inc
http://schema.org/description
- "The High-Lift Flight Tunnel (HiLiFT) concept is a revolutionary approach to aerodynamic ground testing. This concept utilizes magnetic, levitation and linear motors to propel an aerodynamic model through a tube containing a quiescent test medium. This medium (nitrogen) is cryogenic and pressurized to achieve full flight Reynolds numbers higher than any existing ground test facility world-wide for the range of 0.05 to 0.50 Mach. The results of the Phase II study provide excellent assurance that the HiLiFT concept will provide a valuable low-speed, high Reynolds number ground test facility. The design studies concluded that the HiLiFT facility is feasible to build and operate and the analytical studies revealed no insurmountable difficulties to realizing a practical high Reynolds number ground test facility."@en