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Passive venting technique for shallow cavitiesA device is introduced for reducing drag and store separation difficulties caused by shallow cavities on aircraft in supersonic flight consisting of a group of hollow pipes the same length as the cavity. The pipes are attached to the cavity floor so as to allow air to flow through the pipes. This device allows air to flow through the pipes opposite to the direction of flow outside the pipes. This results in reduced drag and improved store separation characteristics.
Document ID
19900010763
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Stallings, Robert L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Wilcox, Floyd J., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
September 5, 1989
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-252081
Patent Number: NASA-CASE-LAR-14031-1
Patent Number: US-PATENT-4,863,118
Accession Number
90N20079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-14031-1|US-PATENT-4,863,118
Patent Application
US-PATENT-APPL-SN-252081
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