• The engine pressure ratio (EPR) is the total pressure ratio across a jet engine, measured as the ratio of the total pressure at the exit of the propelling...
    2 KB (204 words) - 17:01, 9 June 2024
  • turbine engine. The terms compression ratio and pressure ratio are used interchangeably. Overall compression ratio also means the overall cycle pressure ratio...
    6 KB (795 words) - 20:09, 7 July 2024
  • Thumbnail for Turbofan
    of the engine by increasing its pressure ratio or turbine temperature to achieve better combustion causes a corresponding increase in pressure and temperature...
    92 KB (11,155 words) - 16:00, 24 September 2024
  • Pressure ratio may refer to: Compression ratio, for piston engines Overall pressure ratio, for gas turbine engines Pressure ratio, the compression ratio...
    211 bytes (58 words) - 16:02, 29 November 2020
  • Thumbnail for Bypass ratio
    described in terms of BPR, which together with engine pressure ratio, turbine inlet temperature and fan pressure ratio are important design parameters. In addition...
    28 KB (2,122 words) - 14:40, 26 September 2024
  • Thumbnail for Compression ratio
    The compression ratio is the ratio between the volume of the cylinder and combustion chamber in an internal combustion engine at their maximum and minimum...
    13 KB (1,631 words) - 16:33, 26 September 2024
  • Thumbnail for Afterburner
    it pays to select an engine cycle with a high specific thrust (i.e. high fan pressure ratio/low bypass ratio). The resulting engine is relatively fuel efficient...
    20 KB (2,619 words) - 23:59, 21 August 2024
  • Thumbnail for Components of jet engines
    high pressure ratios (e.g. 10:1), impeller stress considerations limit the pressure ratio that can be employed in high overall pressure ratio engine cycles...
    46 KB (6,646 words) - 00:53, 1 October 2024
  • Thumbnail for Compressor stall
    can occur during the operation of the engine to lower the surge pressure ratio or raise the operating pressure ratio. When the two coincide there is no longer...
    16 KB (2,212 words) - 00:04, 19 June 2024
  • Thumbnail for Rotating detonation engine
    A rotating detonation engine (RDE) uses a form of pressure gain combustion, where one or more detonations continuously travel around an annular channel...
    19 KB (1,968 words) - 07:25, 18 July 2024
  • Thumbnail for Jet engine
    exit area is the correct value for the nozzle pressure ratio (npr). Since the npr changes with engine thrust setting and flight speed this is seldom...
    61 KB (7,824 words) - 03:53, 23 September 2024
  • Thumbnail for Ramjet
    Ramjet (redirect from Ramjet engine)
    bypass engine can be described as transitioning from turbo to ramjet mode if it can attain a flight speed at which the engine pressure ratio (epr) has...
    36 KB (4,882 words) - 14:08, 13 September 2024
  • Thumbnail for Aerospike engine
    Ambient air pressure also imparts a small pressure against the exhaust, helping to keep it moving in the "right" direction as it exits the engine. As the...
    23 KB (2,543 words) - 09:24, 27 September 2024
  • Thumbnail for Pulsejet
    Pulsejet (redirect from Pulse jet engine)
    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...
    27 KB (3,662 words) - 19:08, 24 August 2024
  • and fuel consumption) for a pilot is displayed in the cockpit as engine pressure ratio (EPR) and exhaust gas temperature (EGT) or fan speed (N1) and EGT...
    118 KB (16,905 words) - 16:41, 22 September 2024
  • Thumbnail for Rocket engine
    expansion-ratio. The large bell- or cone-shaped nozzle extension beyond the throat gives the rocket engine its characteristic shape. The exit static pressure of...
    100 KB (11,709 words) - 16:03, 2 October 2024
  • Thumbnail for Turbojet
    Turbojet (redirect from Turbojet engine)
    powerplant efficiency (the engine efficiency is increased by the ram pressure rise which adds to the compressor pressure rise, the higher aircraft speed...
    28 KB (3,494 words) - 20:14, 30 September 2024
  • The Coffman engine starter (also known as a "shotgun starter") was a starting system used on many piston engines in aircraft and armored vehicles of the...
    5 KB (729 words) - 15:29, 30 August 2024
  • Thumbnail for Gas turbine engine compressors
    disadvantage. At high overall pressure ratios, the compression system is usually split into two units; a low-pressure (LP) compressor mounted on one...
    6 KB (756 words) - 07:12, 25 October 2023
  • Thumbnail for Variable cycle engine
    mode the engine acts more like a 'leaky' turbojet (e.g. the F404). In the mixed-flow turbofan with ejector concept, a low bypass ratio engine is mounted...
    8 KB (1,053 words) - 06:52, 24 May 2024
  • Thumbnail for Turboshaft
    Turboshaft (redirect from Turboshaft engine)
    multiple-ratio transmissions and clutches. An unusual example of the turboshaft principle is the Pratt & Whitney F135-PW-600 turbofan engine for the STOVL...
    7 KB (794 words) - 10:53, 24 October 2023
  • Thumbnail for Rolls-Royce/Snecma Olympus 593
    included thrust-specific fuel consumption (TSFC or simply SFC), engine pressure ratio, size and weight, and turbine entry temperature. Initial studies...
    27 KB (3,080 words) - 04:58, 4 May 2024
  • Thumbnail for Aircraft engine
    an overall engine efficiency of 48.2%, for a burner temperature of 1,700 K (1,430 °C), an overall pressure ratio of 38 and a peak pressure of 30 MPa (300 bar)...
    43 KB (5,236 words) - 14:13, 25 September 2024
  • start large diesel engines and gas turbines. Compared to a gasoline (petrol) engine, a diesel engine has a very high compression ratio, an essential design...
    9 KB (1,224 words) - 04:34, 29 February 2024
  • expansion ratio. For any heat engine the work which can be extracted from it is proportional to the difference between the starting pressure and the ending...
    28 KB (3,874 words) - 15:02, 1 October 2024
  • Thumbnail for Pressure-fed engine
    The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and...
    6 KB (547 words) - 09:20, 27 September 2024
  • Thumbnail for Steam engine
    steam engine is a heat engine that performs mechanical work using steam as its working fluid. The steam engine uses the force produced by steam pressure to...
    78 KB (9,749 words) - 11:05, 17 September 2024
  • Thumbnail for Aircraft engine starting
    piston engine gas starting system, used on the Bristol Jupiter engine in 1922. A system used in early Rolls-Royce Kestrel engines ducted high-pressure air...
    19 KB (2,353 words) - 21:20, 30 September 2024
  • Thumbnail for Axial compressor
    bleed). Modern jet engines use a series of compressors, running at different speeds; to supply air at around 40:1 pressure ratio for combustion with...
    33 KB (5,121 words) - 09:24, 9 July 2024
  • valve mechanism of a conventional engine, which may reduce mechanical complexity and enable an increased compression ratio by eliminating hotspots that would...
    25 KB (3,207 words) - 23:15, 29 September 2024