Category:Aerodynamics
Przejdź do nawigacji
Przejdź do wyszukiwania
ruchy gazów, powstające przy tym siły  Adenydd awyren yn creu trobwyll | |||||
| Prześlij plik multimedialny | |||||
| Jest to |
| ||||
|---|---|---|---|---|---|
| Podklasa dla |
| ||||
| |||||
 | |||||
English: 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.
Podkategorie
Poniżej wyświetlono 29 spośród wszystkich 29 podkategorii tej kategorii.
*
A
- Aeroelasticity (6 plików)
C
- Camber (aerodynamics) (9 plików)
F
- Flow conditioning (1 plik)
- Formula One cars with flow visualization paint (17 plików)
G
R
- Rollerons (16 plików)
S
- Steady transonic gas flow equation simulation (17 plików)
V
W
Pliki w kategorii „Aerodynamics”
Poniżej wyświetlono 127 spośród wszystkich 127 plików w tej kategorii.
-
3840x1080 F16 OpenFOAM.jpg 3840 × 1080; 2,73 MB
-
Aerodinamika1.png 786 × 386; 100 KB
-
Aerodynamic data of Aerofoil BET.svg 596 × 385; 109 KB
-
Aerodynamic forces BET.svg 504 × 348; 36 KB
-
Aerodynamic forces on a body, captioned.svg 333 × 220; 8 KB
-
Aerodynamic-forces-illustration.jpg 715 × 427; 90 KB
-
Aerodynamically efficient gradient refractive index missile seeker lens. (IA aerodynamicallye00carr).pdf 1145 × 1547, 978 stron; 23,97 MB
-
Aerodynamic analysis of a U.S. Navy and Marine Corps unmanned air vehicle. (IA aerodynamicanaly00lyon).pdf 1208 × 1556, 214 stron; 9,41 MB
-
Aerodynamic analysis of a modified, pylon-mounted JSOW (IA aerodynamicanaly00pome).pdf 1200 × 1595, 202 strony; 7,46 MB
-
Aerodynamic coefficients of a symmetrical airfoil in an oscillating flow (IA aerodynamiccoeff1094510801).pdf 1275 × 1650, 102 strony; 2,79 MB
-
Aerodynamic design of symmetrical blading for three-stage axial flow compressor test rig (IA aerodynamicdesig00vavr).pdf 1150 × 1602, 66 stron; 3,62 MB
-
Aerodynamic design using parallel processors (IA aerodynamicdesig1094539914).pdf 1275 × 1650, 153 strony; 4,39 MB
-
Aerodynamic loads on a ball-obturated tubular projectile. (IA aerodynamicloads00bryw).pdf 1191 × 1566, 148 stron; 4,05 MB
-
Aerodynamic analysis of a canard missile configuration using ANSYS-CFX (IA aerodynamicnalys1094510707).pdf 1275 × 1650, 116 stron; 4,62 MB
-
Aerodynamic analysis of M33 projectile using the CFX code (IA aerodynamicnalys1094510711).pdf 1275 × 1650, 98 stron; 2,4 MB
-
-
-
Aerodynamic performance predictions of a SA-2 Missile using Missile Datcom (IA aerodynamicperfo109454578).pdf 1275 × 1650, 78 stron; 911 KB
-
-
Aerodynamics Forces.jpg 259 × 194; 9 KB
-
Aerodynamic stabilization of an electrical discharge for gas lasers. (IA aerodynamicstabi00davi).pdf 1172 × 1602, 214 stron; 5,98 MB
-
Aerodynamic Validation of Emerging Projectile Configurations (IA aerodynamicvalid1094514852).pdf 1275 × 1650, 104 strony; 4,58 MB
-
Aerodynamic validation of emerging projectile and missile configurations (IA aerodynamicvalid109454979).pdf 1275 × 1650, 110 stron; 2,04 MB
-
Aircraft Angle of Incidence (improved)--1080x660--25Mar2009.jpg 1080 × 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 1350 × 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 × 1021; 86 KB
-
Boatforcestop.svg 1012 × 629; 44 KB
-
Bulk aerodynamic formulas.jpg 621 × 578; 55 KB
-
Bypass transition.png 1920 × 1196; 37 KB
-
Chart for equation BET.png 595 × 806; 694 KB
-
Chart for sollution of O BET.png 644 × 809; 538 KB
-
Coefficients of Lift and Drag for a Hypothetical Sail.png 720 × 540; 78 KB
-
Convex lower chamber BET.svg 460 × 300; 33 KB
-
Cp au flanc d'un fuselage d'avion de transport.png 1050 × 776; 96 KB
-
-
CPA de corps profilés selon Hoerner Lift, 19-20 fig. 31.png 885 × 863; 40 KB
-
DartNbeta.svg 800 × 600; 54 KB
-
DartNr.svg 800 × 600; 26 KB
-
DartYbeta.svg 800 × 600; 15 KB
-
Delta-wing-vortex.jpg 749 × 619; 179 KB
-
DiagCollar.jpg 1159 × 875; 66 KB
-
Diagram BED.svg 464 × 308; 26 KB
-
DiagramaCollar.jpg 600 × 452; 40 KB
-
Dihedral angle farsi.png 4632 × 2872; 46 KB
-
Downwash corrections e BET.png 644 × 933; 405 KB
-
Dynamische windvleugel 2 bladen op tandem (polyphon).jpg 2400 × 2000; 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
-
Grand manège de Maxim.tif 1549 × 1002; 1,47 MB
-
Gripit Optimisation.jpg 1440 × 1440; 186 KB
-
Horsepower required for various speeds.png 1000 × 640; 4 KB
-
Karman-Vortex.gif 850 × 478; 9,74 MB
-
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
-
-
-
-
MissileDynamics.svg 800 × 600; 35 KB
-
Motocorsa 24 0070 - Ducati V4R.jpg 2000 × 1333; 703 KB
-
Motocorsa 24 0073 - Ducati V4R.jpg 2000 × 1333; 700 KB
-
Motocorsa 24 0078 - Ducati V4R.jpg 2000 × 1333; 623 KB
-
Multiplane BET.svg 562 × 325; 1,08 MB
-
MUNK REVISITED.jpg 1369 × 587; 870 KB
-
Möwenflug (Dünenkette).webm 1 min 19 s, 1920 × 1080; 13,38 MB
-
Möwenflug (Schiffsheck).webm 58 s, 1920 × 1080; 13,95 MB
-
-
New generation Jet Blast deflector.jpg 4809 × 2929; 11,37 MB
-
OPTIMAL AERODYNAMIC EFFICIENCY RATIO.jpg 3239 × 1709; 2,26 MB
-
Ordinates BET.svg 491 × 118; 34 KB
-
Particle Tracking Velocimetry.png 667 × 472; 89 KB
-
Percolat, ailerons multitubulaires.jpg 522 × 1032; 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 3346 × 1998; 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 1200 × 900; 99 KB
-
Rep pde fig2.jpeg 1200 × 900; 92 KB
-
Rep pde fig3.jpeg 1200 × 900; 94 KB
-
Rep pde fig4.jpeg 1200 × 900; 103 KB
-
Richtung640.png 800 × 578; 102 KB
-
Rough sketch of isobar pattern around a lifting airfoil.jpg 3456 × 4608; 141 KB
-
Screenshot MIRAS-FLEX direct.png 1201 × 752; 554 KB
-
Sens de l'effet Magnus, gauche.png 1009 × 657; 37 KB
-
Sens effet Magnus.png 1009 × 655; 32 KB
-
Smooth Finish Makes Smooth Flying Art.IWMPST14268.jpg 472 × 716; 37 KB
-
Standard propeller sections 2 BET.png 626 × 728; 553 KB
-
Stolperkante, Vortexgenerator und Überziehwarneinrichtung an Aquila A210.jpg 4000 × 3000; 3,27 MB
-
Streamline Patterns for Flow Regimes.png 1202 × 1362; 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 5184 × 3456; 9,34 MB
-
Trajectory3.JPG 5184 × 3456; 4,55 MB
-
Transsonic flow1.png 1214 × 527; 22 KB
-
TucanSnapshot.png 1600 × 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
-
Voiture profilée de H. G Reid, Popular Mechanics Mag., Mars 1936.png 571 × 340; 283 KB
-
Voiture profilée de H. G. Reid, thèse Eyolfson.png 1182 × 716; 191 KB
-
Voiture profilée de H. G. Reid, thèse Eyolfson2.png 1056 × 677; 92 KB
-
Vortilons on a Cozy MKIV.jpg 3491 × 2765; 1,7 MB
-
Windvleugel 2 bladen haaks op een as met veerdemping (comtoise klok).jpg 2400 × 1800; 2,29 MB
-
Wing 2 BET.svg 564 × 279; 35 KB
-
Wing profile nomenclature (pl).svg 1022 × 433; 23 KB
-
Диаграмма загрузка-дальность, Boeing 787-9.png 1133 × 752; 110 KB
-
Пикирование самолёта схема..jpg 1260 × 1080; 83 KB
-
Срыв пограничного слоя.jpg 5100 × 3108; 800 KB
-
Характерные точки диаграммы загрузка-дальность.png 535 × 304; 8 KB
--1080x660--25Mar2009.jpg)
.jpg)
.jpg)
.svg)
