Category:Compressible flow
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English: Compressible flow is the area of fluid mechanics that deals with fluids in which the fluid density varies significantly in response to a change in pressure.
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Subcategories
This category has the following 9 subcategories, out of 9 total.
A
D
F
- Fanno flow (8 F)
M
- Mach number (21 F)
P
- Prandtl–Meyer expansion fans (2 F)
R
- Rayleigh flow (3 F)
S
Media in category "Compressible flow"
The following 66 files are in this category, out of 66 total.
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Aerodynamic relations for delta wings 1.jpg 1,848 × 909; 92 KB
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Aerodynamic relations for delta wings 2.png 1,848 × 848; 40 KB
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Buseman.svg 609 × 196; 5 KB
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Ceoni udarni talas.svg 1,117 × 1,229; 23 KB
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Choked flow.png 622 × 391; 36 KB
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Compressible Airflow Airplane.jpg 600 × 400; 86 KB
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Deviazioneflussosupersonico2.PNG 245 × 131; 3 KB
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Drag factor.svg 598 × 556; 12 KB
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Explanation of Sonic Motion.png 1,242 × 923; 60 KB
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Fan, before 1945.jpg 4,128 × 2,322; 2.8 MB
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Fanno flow.JPG 1,247 × 630; 45 KB
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Fig 27 5.JPG 499 × 369; 13 KB
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Flowpatterns.gif 344 × 916; 16 KB
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Fonction Prandtl-Meyer.png 771 × 771; 6 KB
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GB528 CD.jpg 1,132 × 788; 187 KB
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Grah chocking.jpg 960 × 720; 24 KB
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Isentropic Flow Relations Table.PNG 649 × 500; 20 KB
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Krozzvucno strujanje.svg 1,500 × 804; 14 KB
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Mach angle.jpg 1,185 × 672; 45 KB
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MM pv plane 01.png 906 × 810; 67 KB
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MM pv plane 02.svg 1,280 × 720; 101 KB
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MM pv plane 03.png 901 × 815; 67 KB
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Non-ideal nozzle 01.png 992 × 623; 121 KB
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Non-ideal nozzle 02.svg 1,280 × 720; 65 KB
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Nose cone bi-conic.png 401 × 160; 7 KB
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Oblique Shock Wave.JPG 537 × 436; 21 KB
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Onda de choque2.jpg 506 × 177; 24 KB
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Perfil Cx divergencia.png 300 × 328; 18 KB
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Poremecaj stoji a).svg 1,052 × 1,052; 25 KB
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Prandtl meyer function.png 1,212 × 825; 32 KB
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Prandtl-Glauert singularity-en.svg 720 × 580; 5 KB
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Prandtl-Glauert singularity-fr.svg 720 × 580; 5 KB
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Prandtl-Glauert singularity.svg 720 × 580; 5 KB
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Pressure wave 2.svg 1,295 × 803; 21 KB
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Pressure wave.svg 1,188 × 449; 15 KB
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Profil aile supersonique.png 314 × 206; 5 KB
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Profil im Transschall.JPG 972 × 497; 28 KB
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Profil im Ueberschall.JPG 1,014 × 705; 42 KB
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Properties isentropic supersonic expansion.svg 816 × 557; 10 KB
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Qualitive variation of cd with mach number.png 450 × 320; 13 KB
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Rankine-Hugoniot Relationships.PNG 508 × 333; 13 KB
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Schema Prandtl-Meyer.png 744 × 1,052; 34 KB
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Shock Reflection.jpg 444 × 230; 608 KB
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Shock wave control volume.svg 1,090 × 342; 21 KB
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Sub-Supersonic Diffusers and Nozzles.png 1,326 × 1,065; 57 KB
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Subsonic and trans-sonic airfoils.svg 1,297 × 1,954; 19 KB
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Subsonic vs. supersonic flow behaviors.svg 1,420 × 1,137; 17 KB
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Supersonic Free-Flight Wind Tunnel (9416058938).jpg 3,237 × 2,495; 734 KB
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Supersonic Free-Flight Wind Tunnel (9416059462).jpg 2,409 × 2,708; 291 KB
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Supersonic Free-Flight Wind Tunnel (9416945766).jpg 3,000 × 2,399; 883 KB
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Supersonic Free-Flight Wind Tunnel (9416948964).jpg 3,218 × 2,360; 1.07 MB
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Supersonic.svg 518 × 317; 9 KB
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SWT alt.JPG 772 × 198; 23 KB
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Transonic flow patterns it.svg 286 × 234; 39 KB
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Transsonic flow over airfoil 1.gif 220 × 87; 2 KB
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Transsonic flow over airfoil 1.svg 206 × 87; 8 KB
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Transsonic flow over airfoil 2.gif 221 × 133; 2 KB
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Transsonic flow over airfoil 2.svg 229 × 136; 7 KB
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Uglovi strujnica.svg 1,500 × 825; 21 KB
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Undebalistice.jpg 622 × 311; 40 KB
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UnghiulMach.jpg 622 × 311; 30 KB
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Voilure supercritique.svg 351 × 399; 20 KB
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Wedge1.PNG 691 × 363; 12 KB
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Www.grc.nasa.gov.gif 708 × 530; 13 KB
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