wetted area
1Wetted area — In sailboating, the wetted area is the area of the hull which is immersed in water. References …
2wetted area — upės skerspjūvio plotas statusas Aprobuotas sritis hidrometeorologija apibrėžtis Plotas upės tekėjimo krypčiai statmenos plokštumos, kurią iš apačios riboja dugnas, iš šonų – vagos šlaitai, o iš viršaus – vandens paviršius. atitikmenys: angl.… …
3wetted area — vilgomasis plotas statusas T sritis fizika atitikmenys: angl. wetted area vok. benetzte Fläche, f rus. смачиваемая площадь, f pranc. aire mouillée, f …
4wetted area — The cross sectional area of that portion of a channel that is filled with water [16] …
5Wetted perimeter — The wetted perimeter is the perimeter of the cross sectional area that is wet. The term wetted perimeter is common in Civil Engineering, Environmental Engineering and heat transfer applications; it is associated with the hydraulic diameter.… …
6Wetted aspect ratio (wing) — The wetted aspect ratio is a good indication of the aerodynamic efficiency of an aircraft. It is a better measure than the aspect ratio. It is defined as:: ARwet = {b^2 over Sw} where Sw is the wetted surface of the whole aircraft in contrast to… …
7Darcy–Weisbach equation — In fluid dynamics, the Darcy–Weisbach equation is a phenomenological equation, which relates the head loss or pressure loss due to friction along a given length of pipe to the average velocity of the fluid flow. The equation is named after Henry… …
8Wing configuration — For aircraft configurations in general, including fuselage, tail and powerplant configuration, see Aircraft. For rotary winged aircraft types, see Rotorcraft. For direct lift and compound or hybrid types, see Powered lift. Fixed wing aircraft,… …
9Darcy-Weisbach equation — The Darcy Weisbach equation is an important and widely used phenomenological equation in hydraulics. It relates the head loss or pressure loss due to friction along a given length of pipe to the average velocity of the fluid flow. Head loss form… …
10Nose cone design — Given the problem of the aerodynamic design of the nose cone section of any vehicle or body meant to travel through a compressible fluid medium (such as a rocket or aircraft, missile or bullet), an important problem is the determination of the… …
