Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Overall_pressure_ratio> ?p ?o }
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- Overall_pressure_ratio abstract "In aeronautical engineering, overall pressure ratio is the ratio of the stagnation pressure as measured at the front and rear of the compressor of a gas turbine engine. Generally speaking, a higher overall pressure ratio implies higher efficiency, but the engine will usually weigh more, so there is a compromise.".
- Overall_pressure_ratio wikiPageID "7495406".
- Overall_pressure_ratio wikiPageLength "6054".
- Overall_pressure_ratio wikiPageOutDegree "50".
- Overall_pressure_ratio wikiPageRevisionID "677793629".
- Overall_pressure_ratio wikiPageWikiLink Aeronautical_engineering.
- Overall_pressure_ratio wikiPageWikiLink Aerospace_engineering.
- Overall_pressure_ratio wikiPageWikiLink Airbus_A300.
- Overall_pressure_ratio wikiPageWikiLink Airbus_A350_XWB.
- Overall_pressure_ratio wikiPageWikiLink Airbus_A380.
- Overall_pressure_ratio wikiPageWikiLink Boeing_747.
- Overall_pressure_ratio wikiPageWikiLink Boeing_767.
- Overall_pressure_ratio wikiPageWikiLink Boeing_777.
- Overall_pressure_ratio wikiPageWikiLink Brayton_cycle.
- Overall_pressure_ratio wikiPageWikiLink Carnot_cycle.
- Overall_pressure_ratio wikiPageWikiLink Category:Engineering_ratios.
- Overall_pressure_ratio wikiPageWikiLink Category:Gas_turbines.
- Overall_pressure_ratio wikiPageWikiLink Combined_gas_law.
- Overall_pressure_ratio wikiPageWikiLink Compression_ratio.
- Overall_pressure_ratio wikiPageWikiLink Concorde.
- Overall_pressure_ratio wikiPageWikiLink Engine_pressure_ratio.
- Overall_pressure_ratio wikiPageWikiLink Figure_of_merit.
- Overall_pressure_ratio wikiPageWikiLink Gas_turbine.
- Overall_pressure_ratio wikiPageWikiLink General_Dynamics_F-111.
- Overall_pressure_ratio wikiPageWikiLink General_Dynamics_F-111_Aardvark.
- Overall_pressure_ratio wikiPageWikiLink General_Dynamics_F-16_Fighting_Falcon.
- Overall_pressure_ratio wikiPageWikiLink General_Electric_CF6.
- Overall_pressure_ratio wikiPageWikiLink General_Electric_F110.
- Overall_pressure_ratio wikiPageWikiLink General_Electric_GE90.
- Overall_pressure_ratio wikiPageWikiLink Grumman_F-14_Tomcat.
- Overall_pressure_ratio wikiPageWikiLink HVAC.
- Overall_pressure_ratio wikiPageWikiLink Heating_load.
- Overall_pressure_ratio wikiPageWikiLink Junkers_Jumo_004.
- Overall_pressure_ratio wikiPageWikiLink Lockheed_C-5_Galaxy.
- Overall_pressure_ratio wikiPageWikiLink McDonnell_Douglas_F-15_Eagle.
- Overall_pressure_ratio wikiPageWikiLink McDonnell_Douglas_MD-11.
- Overall_pressure_ratio wikiPageWikiLink Otto_cycle.
- Overall_pressure_ratio wikiPageWikiLink Pratt_&_Whitney_F135.
- Overall_pressure_ratio wikiPageWikiLink Pratt_&_Whitney_TF30.
- Overall_pressure_ratio wikiPageWikiLink Pressure.
- Overall_pressure_ratio wikiPageWikiLink Reciprocating_engine.
- Overall_pressure_ratio wikiPageWikiLink Rocket_engine.
- Overall_pressure_ratio wikiPageWikiLink Snecma_Olympus_593.
- Overall_pressure_ratio wikiPageWikiLink Rolls-Royce_Trent.
- Overall_pressure_ratio wikiPageWikiLink Rolls-Royce_Trent_XWB.
- Overall_pressure_ratio wikiPageWikiLink SNECMA_Atar.
- Overall_pressure_ratio wikiPageWikiLink Sea_level.
- Overall_pressure_ratio wikiPageWikiLink Space_Shuttle_Main_Engine.
- Overall_pressure_ratio wikiPageWikiLink Space_Shuttle_main_engine.
- Overall_pressure_ratio wikiPageWikiLink Stagnation_pressure.
- Overall_pressure_ratio wikiPageWikiLink Thrust_specific_fuel_consumption.
- Overall_pressure_ratio wikiPageWikiLink World_War_II.
- Overall_pressure_ratio wikiPageWikiLinkText "Overall pressure ratio".
- Overall_pressure_ratio wikiPageWikiLinkText "Pressure ratio".
- Overall_pressure_ratio wikiPageWikiLinkText "compression ratio".
- Overall_pressure_ratio wikiPageWikiLinkText "overall pressure ratio".
- Overall_pressure_ratio wikiPageWikiLinkText "pressure ratio".
- Overall_pressure_ratio hasPhotoCollection Overall_pressure_ratio.
- Overall_pressure_ratio wikiPageUsesTemplate Template:Refimprove.
- Overall_pressure_ratio wikiPageUsesTemplate Template:Reflist.
- Overall_pressure_ratio subject Category:Engineering_ratios.
- Overall_pressure_ratio subject Category:Gas_turbines.
- Overall_pressure_ratio hypernym Ratio.
- Overall_pressure_ratio type Aircraft.
- Overall_pressure_ratio type Article.
- Overall_pressure_ratio type Article.
- Overall_pressure_ratio type Concept.
- Overall_pressure_ratio type Ratio.
- Overall_pressure_ratio type Technology.
- Overall_pressure_ratio type Turbine.
- Overall_pressure_ratio comment "In aeronautical engineering, overall pressure ratio is the ratio of the stagnation pressure as measured at the front and rear of the compressor of a gas turbine engine. Generally speaking, a higher overall pressure ratio implies higher efficiency, but the engine will usually weigh more, so there is a compromise.".
- Overall_pressure_ratio label "Overall pressure ratio".
- Overall_pressure_ratio sameAs Ciśnienie_sprężania.
- Overall_pressure_ratio sameAs m.0263gkv.
- Overall_pressure_ratio sameAs Tlačno_razmerje.
- Overall_pressure_ratio sameAs Q7113544.
- Overall_pressure_ratio sameAs Q7113544.
- Overall_pressure_ratio wasDerivedFrom Overall_pressure_ratio?oldid=677793629.
- Overall_pressure_ratio isPrimaryTopicOf Overall_pressure_ratio.