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- Thermodynamic_relations_across_normal_shocks abstract "\"Normal shocks\" are a fundamental type of shock wave. The waves, which are perpendicular to the flow, are called \"normal\" shocks. Normal shocks only happen when the flow is supersonic. At those speeds, no obstacle is identified before the speed of sound which makes the molecule return after sensing the obstacle. While returning, the molecule becomes coalescent at certain point. This thin film of molecules act as normal shocks.".
- Thermodynamic_relations_across_normal_shocks wikiPageID "39698985".
- Thermodynamic_relations_across_normal_shocks wikiPageLength "2080".
- Thermodynamic_relations_across_normal_shocks wikiPageOutDegree "4".
- Thermodynamic_relations_across_normal_shocks wikiPageRevisionID "695185659".
- Thermodynamic_relations_across_normal_shocks wikiPageWikiLink Category:Shock_waves.
- Thermodynamic_relations_across_normal_shocks wikiPageWikiLink Mach_number.
- Thermodynamic_relations_across_normal_shocks wikiPageWikiLink Shock_wave.
- Thermodynamic_relations_across_normal_shocks wikiPageWikiLink Supersonic_speed.
- Thermodynamic_relations_across_normal_shocks wikiPageWikiLinkText "Thermodynamic relations across normal shocks".
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:Cite_book.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:Clarify.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:EquationRef.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:Multiple_issues.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:NumBlk.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:Orphan.
- Thermodynamic_relations_across_normal_shocks wikiPageUsesTemplate Template:Technical.
- Thermodynamic_relations_across_normal_shocks subject Category:Shock_waves.
- Thermodynamic_relations_across_normal_shocks hypernym Type.
- Thermodynamic_relations_across_normal_shocks comment "\"Normal shocks\" are a fundamental type of shock wave. The waves, which are perpendicular to the flow, are called \"normal\" shocks. Normal shocks only happen when the flow is supersonic. At those speeds, no obstacle is identified before the speed of sound which makes the molecule return after sensing the obstacle. While returning, the molecule becomes coalescent at certain point. This thin film of molecules act as normal shocks.".
- Thermodynamic_relations_across_normal_shocks label "Thermodynamic relations across normal shocks".
- Thermodynamic_relations_across_normal_shocks sameAs Q18394128.
- Thermodynamic_relations_across_normal_shocks sameAs m.0w1f6gp.
- Thermodynamic_relations_across_normal_shocks sameAs Q18394128.
- Thermodynamic_relations_across_normal_shocks wasDerivedFrom Thermodynamic_relations_across_normal_shocks?oldid=695185659.
- Thermodynamic_relations_across_normal_shocks isPrimaryTopicOf Thermodynamic_relations_across_normal_shocks.