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Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
An symmetric "penshape" exit was designed by the method of characteristics for a nozzle pressure of 15. This configuration was experimentally evaluated in quiescent-air tests over a range of pressure ratios from 4 to 16. In an attempt to achieve throat-area modulation, a scheme was also investigated wherein a teardrop-shape ramp moved out of the concave expansion surface to restrict the flow.
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- http://id.loc.gov/authorities/subjects/sh85002635
- http://id.worldcat.org/fast/802370
- http://id.worldcat.org/fast/1171011
- http://id.loc.gov/authorities/subjects/sh85145415
- http://experiment.worldcat.org/entity/work/data/2040661539#Topic/nozzles_design_and_construction
- http://id.loc.gov/authorities/subjects/sh85092916
- http://experiment.worldcat.org/entity/work/data/2040661539#Topic/waste_gases
- http://experiment.worldcat.org/entity/work/data/2040661539#Topic/charts_diagrams_etc
- http://id.worldcat.org/fast/852545
- http://id.worldcat.org/fast/1039827
- http://id.loc.gov/authorities/subjects/sh87002373
- http://experiment.worldcat.org/entity/work/data/2040661539#Topic/air_flow
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- http://worldcat.org/entity/person/id/2722112162
- http://viaf.org/viaf/136563305
- http://experiment.worldcat.org/entity/work/data/2040661539#Organization/united_states_national_advisory_committee_for_aeronautics
- http://viaf.org/viaf/194268699
- http://id.loc.gov/authorities/names/no2015026965
- http://experiment.worldcat.org/entity/work/data/2040661539#Organization/united_states_national_adviosry_committee_for_aeronautics
- http://id.loc.gov/authorities/names/n79060141
- http://experiment.worldcat.org/entity/work/data/2040661539#Organization/lewis_flight_propulsion_laboratory
http://schema.org/description
- "An symmetric "penshape" exit was designed by the method of characteristics for a nozzle pressure of 15. This configuration was experimentally evaluated in quiescent-air tests over a range of pressure ratios from 4 to 16. In an attempt to achieve throat-area modulation, a scheme was also investigated wherein a teardrop-shape ramp moved out of the concave expansion surface to restrict the flow."
- "An symmetric "penshape" exit was designed by the method of characteristics for a nozzle pressure of 15. This configuration was experimentally evaluated in quiescent-air tests over a range of pressure ratios from 4 to 16. In an attempt to achieve throat-area modulation, a scheme was also investigated wherein a teardrop-shape ramp moved out of the concave expansion surface to restrict the flow."@en
http://schema.org/name
- "Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air"
- "Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air"@en