Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q7897510> ?p ?o }
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- Q7897510 subject Q8281165.
- Q7897510 abstract "In supersonic aerodynamics, unstart refers to a generally violent breakdown of the supersonic airflow. The phenomenon occurs when mass flow rate changes significantly within a duct. Avoiding unstarts is a key objective in design of the engine air intakes of supersonic aircraft.".
- Q7897510 thumbnail Inlet_shock_waves_at_Mach_2.jpg?width=300.
- Q7897510 wikiPageWikiLink Q1043944.
- Q7897510 wikiPageWikiLink Q11778649.
- Q7897510 wikiPageWikiLink Q1366187.
- Q7897510 wikiPageWikiLink Q160669.
- Q7897510 wikiPageWikiLink Q170007.
- Q7897510 wikiPageWikiLink Q190114.
- Q7897510 wikiPageWikiLink Q190688.
- Q7897510 wikiPageWikiLink Q2000413.
- Q7897510 wikiPageWikiLink Q221337.
- Q7897510 wikiPageWikiLink Q2917212.
- Q7897510 wikiPageWikiLink Q333195.
- Q7897510 wikiPageWikiLink Q599977.
- Q7897510 wikiPageWikiLink Q6505.
- Q7897510 wikiPageWikiLink Q729056.
- Q7897510 wikiPageWikiLink Q811197.
- Q7897510 wikiPageWikiLink Q8281165.
- Q7897510 wikiPageWikiLink Q8424.
- Q7897510 wikiPageWikiLink Q8995102.
- Q7897510 comment "In supersonic aerodynamics, unstart refers to a generally violent breakdown of the supersonic airflow. The phenomenon occurs when mass flow rate changes significantly within a duct. Avoiding unstarts is a key objective in design of the engine air intakes of supersonic aircraft.".
- Q7897510 label "Unstart".
- Q7897510 depiction Inlet_shock_waves_at_Mach_2.jpg.