Category:Aerodynamics

Potkategorije

Prikazano je 28 potkategorija, od ukupno 28.

Datoteke u kategoriji "Aerodynamics"

Prikazano je 130 datoteka u ovoj kategoriji, od ukupno 130.

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  3840x1080 F16 OpenFOAM.jpg 3.840 × 1.080; 2,73 MB
  
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  Aerodinamika1.png 786 × 386; 100 KB
  
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  Aerodynamic data of Aerofoil BET.svg 596 × 385; 109 KB
  
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  Aerodynamically efficient gradient refractive index missile seeker lens. (IA aerodynamicallye00carr).pdf 1.145 × 1.547, 978 stranica; 23,97 MB
  
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  Aerodynamic analysis of a U.S. Navy and Marine Corps unmanned air vehicle. (IA aerodynamicanaly00lyon).pdf 1.208 × 1.556, 214 stranica; 9,41 MB
  
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  Aerodynamic analysis of a modified, pylon-mounted JSOW (IA aerodynamicanaly00pome).pdf 1.200 × 1.595, 202 stranice; 7,46 MB
  
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  Aerodynamic coefficients of a symmetrical airfoil in an oscillating flow (IA aerodynamiccoeff1094510801).pdf 1.275 × 1.650, 102 stranice; 2,79 MB
  
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  Aerodynamic design of symmetrical blading for three-stage axial flow compressor test rig (IA aerodynamicdesig00vavr).pdf 1.150 × 1.602, 66 stranica; 3,62 MB
  
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  Aerodynamic design using parallel processors (IA aerodynamicdesig1094539914).pdf 1.275 × 1.650, 153 stranice; 4,39 MB
  
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  Aerodynamic loads on a ball-obturated tubular projectile. (IA aerodynamicloads00bryw).pdf 1.191 × 1.566, 148 stranica; 4,05 MB
  
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  Aerodynamic analysis of a canard missile configuration using ANSYS-CFX (IA aerodynamicnalys1094510707).pdf 1.275 × 1.650, 116 stranica; 4,62 MB
  
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  Aerodynamic analysis of M33 projectile using the CFX code (IA aerodynamicnalys1094510711).pdf 1.275 × 1.650, 98 stranica; 2,4 MB
  
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  An aerodynamic performance evaluation of the NASA-Ames Research Center Advanced Concepts Flight Simulator. (IA aerodynamicperfo00dono).pdf 1.187 × 1.558, 122 stranice; 4,94 MB
  
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  Aerodynamic performance of wings of arbitrary planform in inviscid, incompressible, irrotational flow. (IA aerodynamicperfo00holm).pdf 1.189 × 1.560, 230 stranica; 8,47 MB
  
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  Aerodynamic performance predictions of a SA-2 Missile using Missile Datcom (IA aerodynamicperfo109454578).pdf 1.275 × 1.650, 78 stranica; 911 KB
  
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  Aerodynamic predictions, comparisons, and validations using Missilelab and Missile Datcom (97) (IA aerodynamicpredi109453708).pdf 1.275 × 1.650, 52 stranice; 681 KB
  
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  Aerodynamics Forces.jpg 259 × 194; 9 KB
  
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  Aerodynamic stabilization of an electrical discharge for gas lasers. (IA aerodynamicstabi00davi).pdf 1.172 × 1.602, 214 stranica; 5,98 MB
  
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  Aerodynamic Validation of Emerging Projectile Configurations (IA aerodynamicvalid1094514852).pdf 1.275 × 1.650, 104 stranice; 4,58 MB
  
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  Aerodynamic validation of emerging projectile and missile configurations (IA aerodynamicvalid109454979).pdf 1.275 × 1.650, 110 stranica; 2,04 MB
  
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  Aircraft Angle of Incidence (improved)--1080x660--25Mar2009.jpg 1.080 × 660; 108 KB
  
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  Airflow BET.svg 547 × 286; 37 KB
  
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  Airflow propeller BET.svg 828 × 590; 64 KB
  
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  Allometric Law of Body Mass vs Cruising Speed in Constructal Theory.svg 1.350 × 900; 160 KB
  
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  Angle d'incidence.jpg 461 × 300; 12 KB
  
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  Angle màxim en ventall d'extensió de Prandtl-Meyer.png 396 × 350; 11 KB
  
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  Boatforcestern.svg 734 × 1.021; 86 KB
  
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  Boatforcestop.svg 1.012 × 629; 44 KB
  
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  Bulk aerodynamic formulas.jpg 621 × 578; 55 KB
  
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  Bypass transition.png 1.920 × 1.196; 37 KB
  
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  Chart for equation BET.png 595 × 806; 694 KB
  
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  Chart for sollution of O BET.png 644 × 809; 538 KB
  
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  Coefficients of Lift and Drag for a Hypothetical Sail.png 720 × 540; 78 KB
  
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  Convex lower chamber BET.svg 460 × 300; 33 KB
  
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  Cp au flanc d'un fuselage d'avion de transport.png 1.050 × 776; 96 KB
  
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  CPA avant arrière et total d'un corps 3D à deux pointes, Hoener Lift, 19-3 fig. 3.png 1.065 × 672; 34 KB
  
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  CPA de corps profilés selon Hoerner Lift, 19-20 fig. 31.png 885 × 863; 40 KB
  
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  DartNbeta.svg 800 × 600; 54 KB
  
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  DartNr.svg 800 × 600; 26 KB
  
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  DartYbeta.svg 800 × 600; 15 KB
  
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  Delta-wing-vortex.jpg 749 × 619; 179 KB
  
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  DiagCollar.jpg 1.159 × 875; 66 KB
  
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  Diagram BED.svg 464 × 308; 26 KB
  
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  DiagramaCollar.jpg 600 × 452; 40 KB
  
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  Dihedral angle farsi.png 4.632 × 2.872; 46 KB
  
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  Downwash corrections e BET.png 644 × 933; 405 KB
  
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  Dynamische windvleugel 2 bladen op tandem (polyphon).jpg 2.400 × 2.000; 2,32 MB
  
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  Effet Magnus sur cylindre rotatif, d'ap photo de Prandtl.png 980 × 697; 67 KB
  
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  Einstellwinkel640.png 640 × 278; 19 KB
  
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  FallschirmspringerFreierFall.png 640 × 590; 28 KB
  
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  Fig.72.png 441 × 414; 7 KB
  
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  Forces-5.jpg 216 × 146; 7 KB
  
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  Grand manège de Maxim.tif 1.549 × 1.002; 1,47 MB
  
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  Gripit Optimisation.jpg 1.440 × 1.440; 186 KB
  
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  Horsepower required for various speeds.png 1.000 × 640; 4 KB
  
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  Karman-Vortex.gif 850 × 478; 9,74 MB
  
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  Lienhard StrouhalVsReynoldsVortex.jpg 2.746 × 1.459; 1,12 MB
  
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  Lift corrections 8Cl BET.png 861 × 942; 503 KB
  
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  Longitudinal.png 660 × 400; 17 KB
  
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  LowWing.png 800 × 600; 8 KB
  
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  Luchtweerstand roterende windvleugel.jpg 950 × 938; 160 KB
  
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  Mercury-Redstone Center of pressure, The Mercury-Redstone Project NASA TMX 53107.png 442 × 710; 31 KB
  
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  Mercury-Redstone dynamic pressure, The Mercury-Redstone Project NASA TMX 53107.png 540 × 601; 38 KB
  
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  Mercury-Redstone Velocity, The Mercury-Redstone Project NASA TMX 53107.png 630 × 598; 35 KB
  
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  MissileDynamics.svg 800 × 600; 35 KB
  
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  Motocorsa 24 0070 - Ducati V4R.jpg 2.000 × 1.333; 703 KB
  
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  Motocorsa 24 0073 - Ducati V4R.jpg 2.000 × 1.333; 700 KB
  
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  Motocorsa 24 0078 - Ducati V4R.jpg 2.000 × 1.333; 623 KB
  
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  Multiplane BET.svg 562 × 325; 1,08 MB
  
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  MUNK REVISITED.jpg 1.369 × 587; 870 KB
  
• Möwenflug (Dünenkette).webm 1 min 19 s, 1.920 × 1.080; 13,38 MB
  
• Möwenflug (Schiffsheck).webm 58 s, 1.920 × 1.080; 13,95 MB
  
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  New Boeing Method Accelerates Turbulence Modeling Uncertainty Analysis - 38794780404.png 1.395 × 768; 250 KB
  
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  Odchylenie.jpg 1.303 × 1.600; 114 KB
  
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  OPTIMAL AERODYNAMIC EFFICIENCY RATIO.jpg 3.239 × 1.709; 2,26 MB
  
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  Ordinates BET.svg 491 × 118; 34 KB
  
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  Particle Tracking Velocimetry.png 667 × 472; 89 KB
  
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  Percolat, ailerons multitubulaires.jpg 522 × 1.032; 48 KB
  
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  Perfect orifice.JPG 400 × 300; 13 KB
  
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  Planform.png 800 × 600; 10 KB
  
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  Polar diagram of coefficients of lift and drag for angles of attack.png 720 × 540; 66 KB
  
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  Portance théorique et mesurée selon TN 228 et NACA TM 323.gif 693 × 625; 142 KB
  
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  Position of blade pitat BET.svg 717 × 711; 42 KB
  
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  Pressure gradient profile plots above a wing.png 3.600 × 2.760; 98 KB
  
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  Pressure gradient profile plots along an airfoil.png 3.406 × 5.137; 244 KB
  
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  Pressure-Recovery Heb.png 3.346 × 1.998; 193 KB
  
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  Product of inertia.png 800 × 600; 18 KB
  
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  Propeller airfoil characteristics BET.png 630 × 743; 498 KB
  
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  Propeller blade BET.svg 618 × 214; 12 KB
  
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  Propeller R.A.F-6.png 619 × 734; 538 KB
  
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  Propeller RAF-6 12345.png 590 × 829; 622 KB
  
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  Rep pde fig1.jpeg 1.200 × 900; 99 KB
  
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  Rep pde fig2.jpeg 1.200 × 900; 92 KB
  
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  Rep pde fig3.jpeg 1.200 × 900; 94 KB
  
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  Rep pde fig4.jpeg 1.200 × 900; 103 KB
  
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  Richtung640.png 800 × 578; 102 KB
  
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  Rough sketch of isobar pattern around a lifting airfoil.jpg 3.456 × 4.608; 141 KB
  
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  Screenshot MIRAS-FLEX direct.png 1.201 × 752; 554 KB
  
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  Sens de l'effet Magnus, gauche.png 1.009 × 657; 37 KB
  
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  Sens effet Magnus.png 1.009 × 655; 32 KB
  
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  Smooth Finish Makes Smooth Flying Art.IWMPST14268.jpg 472 × 716; 37 KB
  
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  Spostamento degli impalcati dell'Akashi Kaikyō e del Ponte sullo Stretto di Messina..jpg 3.648 × 2.736; 1,7 MB
  
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  Standard propeller sections 2 BET.png 626 × 728; 553 KB
  
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  Stolperkante, Vortexgenerator und Überziehwarneinrichtung an Aquila A210.jpg 4.000 × 3.000; 3,27 MB
  
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  Streamline Patterns for Flow Regimes.png 1.202 × 1.362; 60 KB
  
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  Supersonic flow over a sharp leading edged flat plate at zero incidence.JPG 600 × 331; 19 KB
  
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  Tail plane flying.svg 240 × 100; 6 KB
  
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  Test pressure graph.GIF 671 × 509; 17 KB
  
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  Thrust and torque grading curves BET.svg 536 × 446; 51 KB
  
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  Thrust grading curves BET.svg 657 × 437; 73 KB
  
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  Trajectory2.JPG 5.184 × 3.456; 9,34 MB
  
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  Trajectory3.JPG 5.184 × 3.456; 4,55 MB
  
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  Transsonic flow1.png 1.214 × 527; 22 KB
  
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  TucanSnapshot.png 1.600 × 860; 289 KB
  
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  Two sections BET.svg 603 × 126; 19 KB
  
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  Valve flow coefficient .GIF 400 × 300; 5 KB
  
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  Valve flow coefficient .JPG 400 × 300; 11 KB
  
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  Velocity profile plots along an airfoil.png 3.600 × 2.760; 89 KB
  
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  Voiture profilée de H. G Reid, Popular Mechanics Mag., Mars 1936.png 571 × 340; 283 KB
  
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  Voiture profilée de H. G. Reid, thèse Eyolfson.png 1.182 × 716; 191 KB
  
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  Voiture profilée de H. G. Reid, thèse Eyolfson2.png 1.056 × 677; 92 KB
  
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  Vortilons on a Cozy MKIV.jpg 3.491 × 2.765; 1,7 MB
  
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  Windvleugel 2 bladen haaks op een as met veerdemping (comtoise klok).jpg 2.400 × 1.800; 2,29 MB
  
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  Wing 2 BET.svg 564 × 279; 35 KB
  
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  Wing profile nomenclature (pl).svg 1.022 × 433; 23 KB
  
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  Диаграмма загрузка-дальность, Boeing 787-9.png 1.133 × 752; 110 KB
  
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  Пикирование самолёта схема..jpg 1.260 × 1.080; 83 KB
  
• Свеча за графином.webm 8,1 s, 1.920 × 1.080; 207 KB
  
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  Срыв пограничного слоя.jpg 5.100 × 3.108; 800 KB
  
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  Характерные точки диаграммы загрузка-дальность.png 535 × 304; 8 KB