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  2. Fairchild Republic A-10 Thunderbolt II - Wikipedia

    en.wikipedia.org/wiki/Fairchild_Republic_A-10...

    In service since 1977, it is named after the Republic P-47 Thunderbolt, but is commonly referred to as the "Warthog" or simply "Hog". [3] The A-10 was designed to provide close air support (CAS) to ground troops by attacking enemy armored vehicles, tanks, and other ground forces; it is the only production-built aircraft designed solely for CAS ...

  3. Grumman A-6 Intruder - Wikipedia

    en.wikipedia.org/wiki/Grumman_A-6_Intruder

    Pre-production aircraft, eight built with the first four with rotating jet exhaust pipes, redesignated YA-6A in 1962. [40] A2F-1 First production variant with fixed tailpipe, 484 built, redesignated A-6A in 1962. [40] YA2F-1H Prototype electronic warfare variant, one modified from A2F-1, redesignated YEA-6A in 1962. [40] A2F-1H

  4. Northrop YF-23 - Wikipedia

    en.wikipedia.org/wiki/Northrop_YF-23

    The aircraft had single-expansion ramp nozzles (SERN) and, unlike the YF-22, did not employ thrust vectoring. [29] As on the B-2, the exhaust from the YF-23's engines flowed through troughs in the aft deck to shield the engines from infrared homing (IR) missile detection from below.

  5. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    A propelling nozzle is a nozzle that converts the internal energy of a working gas into propulsive force; it is the nozzle, which forms a jet, that separates a gas turbine, or gas generator, from a jet engine. Propelling nozzles accelerate the available gas to subsonic, transonic, or supersonic velocities depending on the power setting of the ...

  6. Changhe Z-10 - Wikipedia

    en.wikipedia.org/wiki/Changhe_Z-10

    The Changhe Z-10 (Chinese: 直-10; pinyin: Zhí-Shí; lit. 'helicopter-10') is a Chinese medium-weight, twin-turboshaft attack helicopter built by the Changhe Aircraft Industries Corporation for the People's Liberation Army Ground Force.

  7. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    The propelling nozzle converts a gas turbine or gas generator into a jet engine. Power available in the gas turbine exhaust is converted into a high speed propelling jet by the nozzle. The power is defined by typical gauge pressure and temperature values for a turbojet of 20 psi (140 kPa) and 1,000 °F (538 °C). [18]