Category:Aerodynamics
Jump to navigation
Jump to search
 | This is a main category requiring frequent diffusion and maybe maintenance. As many pictures and media files as possible should be moved into appropriate subcategories. |
branch of dynamics concerned with studying the motion of air  Adenydd awyren yn creu trobwyll | |||||
| Upload media | |||||
| Instance of |
| ||||
|---|---|---|---|---|---|
| Subclass of | |||||
| |||||
 | |||||
GND ID: 
Library of Congress authority ID: 
Bibliothèque nationale de France ID: 
U.S. National Archives Identifier: Note that many topics are often studied as part of courses and books on aerodynamics, but in fact belong more generally to the parent Category:Fluid dynamics.
Such topics (e.g. the generation of lift and drag) can be applied to ship propellers, sailboat keels, steam turbines, rocket engine nozzles, etc, where the fluid is not necessarily air. Please consider having a look at Category:Fluid dynamics before adding documents here...
Subcategories
This category has the following 27 subcategories, out of 27 total.
Media in category "Aerodynamics"
The following 114 files are in this category, out of 114 total.
3840x1080 F16 OpenFOAM.jpg 3,840 × 1,080; 2.73 MB
Aerodynamic data of Aerofoil BET.svg 596 × 385; 109 KB
Aerodynamic Forces - Alone and Applied.pdf 1,275 × 1,650, 7 pages; 239 KB
Aerodynamic forces BET.svg 504 × 348; 36 KB
Aerodynamically efficient gradient refractive index missile seeker lens. (IA aerodynamicallye00carr).pdf 1,145 × 1,547, 978 pages; 23.97 MB
Aerodynamic analysis of a U.S. Navy and Marine Corps unmanned air vehicle. (IA aerodynamicanaly00lyon).pdf 1,208 × 1,556, 214 pages; 9.41 MB
Aerodynamic analysis of a modified, pylon-mounted JSOW (IA aerodynamicanaly00pome).pdf 1,200 × 1,595, 202 pages; 7.46 MB
Aerodynamic coefficients of a symmetrical airfoil in an oscillating flow (IA aerodynamiccoeff1094510801).pdf 1,275 × 1,650, 102 pages; 2.79 MB
Aerodynamic design of symmetrical blading for three-stage axial flow compressor test rig (IA aerodynamicdesig00vavr).pdf 1,150 × 1,602, 66 pages; 3.62 MB
Aerodynamic design using parallel processors (IA aerodynamicdesig1094539914).pdf 1,275 × 1,650, 153 pages; 4.39 MB
Aerodynamic loads on a ball-obturated tubular projectile. (IA aerodynamicloads00bryw).pdf 1,191 × 1,566, 148 pages; 4.05 MB
Aerodynamic analysis of a canard missile configuration using ANSYS-CFX (IA aerodynamicnalys1094510707).pdf 1,275 × 1,650, 116 pages; 4.62 MB
Aerodynamic analysis of M33 projectile using the CFX code (IA aerodynamicnalys1094510711).pdf 1,275 × 1,650, 98 pages; 2.4 MB
Aerodynamic performance of wings of arbitrary planform in inviscid, incompressible, irrotational flow. (IA aerodynamicperfo00holm).pdf 1,189 × 1,560, 230 pages; 8.47 MB
Aerodynamic performance predictions of a SA-2 Missile using Missile Datcom (IA aerodynamicperfo109454578).pdf 1,275 × 1,650, 78 pages; 911 KB
Aerodynamics Forces.jpg 259 × 194; 9 KB
Aerodynamic stabilization of an electrical discharge for gas lasers. (IA aerodynamicstabi00davi).pdf 1,172 × 1,602, 214 pages; 5.98 MB
Aerodynamic Validation of Emerging Projectile Configurations (IA aerodynamicvalid1094514852).pdf 1,275 × 1,650, 104 pages; 4.58 MB
Aerodynamic validation of emerging projectile and missile configurations (IA aerodynamicvalid109454979).pdf 1,275 × 1,650, 110 pages; 2.04 MB
Aircraft Angle of Incidence (improved)--1080x660--25Mar2009.jpg 1,080 × 660; 108 KB
Airflow BET.svg 547 × 286; 37 KB
Airflow propeller BET.svg 828 × 590; 64 KB
Allometric Law of Body Mass vs Cruising Speed in Constructal Theory.svg 1,350 × 900; 160 KB
Angle d'incidence.jpg 461 × 300; 12 KB
Angle màxim en ventall d'extensió de Prandtl-Meyer.png 396 × 350; 11 KB
Boatforcestern.svg 734 × 1,021; 86 KB
Boatforcestop.svg 1,012 × 629; 44 KB
Bulk aerodynamic formulas.jpg 621 × 578; 55 KB
Chart for equation BET.png 595 × 806; 694 KB
Chart for sollution of O BET.png 644 × 809; 538 KB
Cityjoule diffuseur.png 2,178 × 1,431; 1.92 MB
Coefficients of Lift and Drag for a Hypothetical Sail.png 720 × 540; 78 KB
Contribution à la traînée pression et friction es.png 966 × 372; 52 KB
Contribution à la traînée pression et friction.png 966 × 372; 49 KB
Convex lower chamber BET.svg 460 × 300; 33 KB
Cp au flanc d'un fuselage d'avion de transport.png 1,050 × 776; 96 KB
CPA de corps profilés selon Hoerner Lift, 19-20 fig. 31.png 885 × 863; 40 KB
Cx d'un autocar d'après formes de l'arrière, Hucho.png 811 × 542; 40 KB
Cx des cars routiers selon formes avant.png 908 × 809; 51 KB
Delta-wing-vortex.jpg 749 × 619; 179 KB
DiagCollar.jpg 1,159 × 875; 66 KB
Diagram BED.svg 464 × 308; 26 KB
DiagramaCollar.jpg 600 × 452; 40 KB
Dihedral angle farsi.png 4,632 × 2,872; 46 KB
Downwash corrections e BET.png 644 × 933; 405 KB
Dynamische windvleugel 2 bladen op tandem (polyphon).jpg 2,400 × 2,000; 2.32 MB
Effet Magnus sur cylindre rotatif, d'ap photo de Prandtl.png 980 × 697; 67 KB
Einstellwinkel640.png 640 × 278; 19 KB
FallschirmspringerFreierFall.png 640 × 590; 28 KB
Fig.72.png 441 × 414; 7 KB
Forces-5.jpg 216 × 146; 7 KB
Gleitwinkel.png 264 × 191; 21 KB
Grand manège de Maxim.tif 1,549 × 1,002; 1.47 MB
HEPIA WT Test Section V4 1.jpg 6,000 × 4,000; 12.37 MB
HEPIA WT Test Section V4 2.jpg 6,000 × 4,000; 8.67 MB
Horsepower required for various speeds.png 1,000 × 640; 4 KB
Le pire.jpg 803 × 532; 90 KB
Lift corrections 8Cl BET.png 861 × 942; 503 KB
Longitudinal.png 660 × 400; 17 KB
LowWing.png 800 × 600; 8 KB
Luchtweerstand roterende windvleugel.jpg 950 × 938; 160 KB
Multiplane BET.svg 562 × 325; 1.08 MB
MUNK REVISITED.jpg 1,369 × 587; 870 KB
OPTIMAL AERODYNAMIC EFFICIENCY RATIO.jpg 3,239 × 1,709; 2.26 MB
Ordinates BET.svg 491 × 118; 34 KB
Percolat, ailerons multitubulaires.jpg 522 × 1,032; 48 KB
Perfect orifice.JPG 400 × 300; 13 KB
Planform.png 800 × 600; 10 KB
Portance théorique et mesurée selon TN 228 et NACA TM 323.gif 693 × 625; 142 KB
Position of blade pitat BET.svg 717 × 711; 42 KB
Pressure-Recovery Heb.png 3,346 × 1,998; 193 KB
Product of inertia.png 800 × 600; 18 KB
Propeller airfoil characteristics BET.png 630 × 743; 498 KB
Propeller blade BET.svg 618 × 214; 12 KB
Propeller R.A.F-6.png 619 × 734; 538 KB
Propeller RAF-6 12345.png 590 × 829; 622 KB
Rep pde fig1.jpeg 1,200 × 900; 99 KB
Rep pde fig2.jpeg 1,200 × 900; 92 KB
Rep pde fig3.jpeg 1,200 × 900; 94 KB
Rep pde fig4.jpeg 1,200 × 900; 103 KB
Richtung640.png 800 × 578; 102 KB
Rough sketch of isobar pattern around a lifting airfoil.jpg 3,456 × 4,608; 141 KB
Sens de l'effet Magnus, gauche.png 1,009 × 657; 37 KB
Sens effet Magnus.png 1,009 × 655; 32 KB
Standard propeller sections 2 BET.png 626 × 728; 553 KB
Stolperkante, Vortexgenerator und Überziehwarneinrichtung an Aquila A210.jpg 4,000 × 3,000; 3.27 MB
Streamline Patterns for Flow Regimes.png 1,202 × 1,362; 60 KB
Tail plane flying.svg 240 × 100; 6 KB
Test pressure graph.GIF 671 × 509; 17 KB
Thrust and torque grading curves BET.svg 536 × 446; 51 KB
Thrust grading curves BET.svg 657 × 437; 73 KB
Trajectory2.JPG 5,184 × 3,456; 9.34 MB
Trajectory3.JPG 5,184 × 3,456; 4.55 MB
Transsonic flow1.png 1,214 × 527; 22 KB
TucanSnapshot.png 1,600 × 860; 289 KB
Two sections BET.svg 603 × 126; 19 KB
Valve flow coefficient .GIF 400 × 300; 5 KB
Valve flow coefficient .JPG 400 × 300; 11 KB
Windvleugel 2 bladen haaks op een as met veerdemping (comtoise klok).jpg 2,400 × 1,800; 2.29 MB
Wing 2 BET.svg 564 × 279; 35 KB
Wing profile nomenclature (pl).svg 1,022 × 433; 23 KB
Диаграмма загрузка-дальность, Boeing 787-9.png 1,133 × 752; 110 KB
Пикирование самолёта схема..jpg 1,260 × 1,080; 83 KB
Срыв пограничного слоя.jpg 5,100 × 3,108; 800 KB
Характерные точки диаграммы загрузка-дальность.png 535 × 304; 8 KB
--1080x660--25Mar2009.jpg)
.jpg)
.jpg)
.svg)
