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Supersonic Elliptical Ramp InletA supersonic inlet includes a supersonic section including a cowl which is at least partially elliptical, a ramp disposed within the cowl, and a flow inlet disposed between the cowl and the ramp. The ramp may also be at least partially elliptical.
Document ID
20160011997
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Adamson, Eric E.
Fink, Lawrence E.
Fugal, Spencer R.
Date Acquired
October 4, 2016
Publication Date
September 20, 2016
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-13/586,247
Patent Number: US-Patent-9,447,731
Funding Number(s)
CONTRACT_GRANT: NNL10AA00T-N+2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,447,731
Patent Application
US-Patent-Appl-SN-13/586,247
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