pulse speed - перевод на голландский
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pulse speed - перевод на голландский

JET ENGINE UTILIZING COMBUSTION IN PULSES TO CREATE JET PROPULSION
Pulse jet; Pulse-Jet Engines; Pulse-jet; Pulse jet engine
  • [[Argus As 014]] pulsejet engine of a V-1 flying bomb at the [[Royal Air Force Museum London]]
  • Animation of a pulsejet engine
  • Pulsejet schematic. First part of the cycle: air flows through the intake (1), and is mixed with fuel (2). Second part: the valve (3) is closed and the ignited fuel-air mix (4) propels the craft.

pulse speed      
polsslag (hartslag)
subsonic speed         
  • Density and pressure decrease smoothly with altitude, but temperature (red) does not. The speed of sound (blue) depends only on the complicated temperature variation at altitude and can be calculated from it since isolated density and pressure effects on the speed of sound cancel each other. The speed of sound increases with height in two regions of the stratosphere and thermosphere, due to heating effects in these regions.
  • 305x305px
  • 305x305px
  • Approximation of the speed of sound in dry air based on the [[heat capacity ratio]] (in green) against the truncated [[Taylor expansion]] (in red).
  • Speed of sound in water vs temperature.
  • Speed of sound as a function of depth at a position north of Hawaii in the [[Pacific Ocean]] derived from the 2005 [[World Ocean Atlas]]. The [[SOFAR channel]] spans the minimum in the speed of sound at about 750-m depth.
DISTANCE TRAVELLED DURING A UNIT OF TIME BY A SOUND WAVE PROPAGATING THROUGH AN ELASTIC MEDIUM
Velocity of sound; Sound speed; Sound velocity; Speed of Sound; Speed Of Sound; Sonic velocity; Subsonic speed; Newton–Laplace equation; Newton-Laplace equation; Sonic speed
snelheid onder de geluidssnelheid, subsone (vlieg)snelheid
sonic speed         
  • Density and pressure decrease smoothly with altitude, but temperature (red) does not. The speed of sound (blue) depends only on the complicated temperature variation at altitude and can be calculated from it since isolated density and pressure effects on the speed of sound cancel each other. The speed of sound increases with height in two regions of the stratosphere and thermosphere, due to heating effects in these regions.
  • 305x305px
  • 305x305px
  • Approximation of the speed of sound in dry air based on the [[heat capacity ratio]] (in green) against the truncated [[Taylor expansion]] (in red).
  • Speed of sound in water vs temperature.
  • Speed of sound as a function of depth at a position north of Hawaii in the [[Pacific Ocean]] derived from the 2005 [[World Ocean Atlas]]. The [[SOFAR channel]] spans the minimum in the speed of sound at about 750-m depth.
DISTANCE TRAVELLED DURING A UNIT OF TIME BY A SOUND WAVE PROPAGATING THROUGH AN ELASTIC MEDIUM
Velocity of sound; Sound speed; Sound velocity; Speed of Sound; Speed Of Sound; Sonic velocity; Subsonic speed; Newton–Laplace equation; Newton-Laplace equation; Sonic speed
geluidssnelheid

Определение

oximeter
[?k's?m?t?]
¦ noun an instrument for measuring the proportion of oxygenated haemoglobin in the blood.
Derivatives
oximetry noun

Википедия

Pulsejet

A pulsejet engine (or pulse jet) is a type of jet engine in which combustion occurs in pulses. A pulsejet engine can be made with few or no moving parts, and is capable of running statically (i.e. it does not need to have air forced into its inlet, typically by forward motion). The best known example may be the Argus As 109-014 used to propel Nazi Germany's V-1 flying bomb.

Pulsejet engines are a lightweight form of jet propulsion, but usually have a poor compression ratio, and hence give a low specific impulse.

There are two main types of pulsejet engines, both of which use resonant combustion and harness the expanding combustion products to form a pulsating exhaust jet that produces thrust intermittently. The first is known as a valved or traditional pulsejet and it has a set of one-way valves through which the incoming air passes. When the air-fuel is ignited, these valves slam shut, which means that the hot gases can only leave through the engine's tailpipe, thus creating forward thrust. The second type of pulsejet is known as the valveless pulsejet. Technically the term for this engine is the acoustic-type pulsejet, or aerodynamically valved pulsejet.

One notable line of research of pulsejet engines includes the pulse detonation engine, which involves repeated detonations in the engine, and which can potentially give high compression and reasonably good efficiency.