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  2. Critical engine - Wikipedia

    en.wikipedia.org/wiki/Critical_engine

    The critical engine of a multi-engine fixed-wing aircraft is the engine that, in the event of failure, would most adversely affect the performance or handling abilities of an aircraft. On propeller aircraft, there is a difference in the remaining yawing moments after failure of the left or the right (outboard) engine when all propellers rotate ...

  3. Minimum control speeds - Wikipedia

    en.wikipedia.org/wiki/Minimum_Control_Speeds

    When an engine on a multi-engine aircraft fails, the thrust distribution on the aircraft becomes asymmetrical, resulting in a yawing moment in the direction of the failed engine. [6] A sideslip develops, causing the total drag of the aircraft to increase considerably, resulting in a drop in the aircraft's rate of climb . [ 7 ]

  4. V speeds - Wikipedia

    en.wikipedia.org/wiki/V_speeds

    The minimum speed that the aircraft is still controllable with the critical engine inoperative [21] while the aircraft is airborne. V MCA is sometimes simply referred to as V MC. V MCG: Minimum control speed ground. The minimum speed that the aircraft is still controllable with the critical engine inoperative [21] while the aircraft is on the ...

  5. List of military fixed wing aircraft in production and in ...

    en.wikipedia.org/wiki/List_of_military_fixed...

    This list of military fixed wing aircraft in production and in development by the European defence industry aims at summarising the current status of the aerospace defence industry in Europe. This list focuses on the Western European military block industry, and excludes Russia, Belarus and Serbia.

  6. P-factor - Wikipedia

    en.wikipedia.org/wiki/P-factor

    P-Factor therefore determines which engine is critical engine. [6] For most aircraft (which have clockwise rotating propellers), the left engine is the critical engine. For aircraft with counter-rotating propellers (i.e. not rotating in the same direction) the P-factor moments are equal and both engines are considered equally critical. Fig. 1.

  7. Jendrassik Cs-1 - Wikipedia

    en.wikipedia.org/wiki/Jendrassik_Cs-1

    György Jendrassik worked on gas turbines and in order to speed up research, he established the Invention Development and Marketing Co. Ltd. in 1936. Following the successful running of a small experimental gas turbine engine of 100 bhp output in 1937, began to design a larger turboprop engine, which would be produced and tested in the Ganz works in Budapest.

  8. Glossary of aerospace engineering - Wikipedia

    en.wikipedia.org/wiki/Glossary_of_aerospace...

    Aircraft flight control systems – A conventional fixed-wing aircraft flight control system consists of flight control surfaces, the respective cockpit controls, connecting linkages, and the necessary operating mechanisms to control an aircraft's direction in flight. Aircraft engine controls are also considered as flight controls as they ...

  9. List of aviation, avionics, aerospace and aeronautical ...

    en.wikipedia.org/wiki/List_of_aviation,_avionics...

    Turbine engine system ACC Accessory In gas turbine engine ACE Actuator control electronics ACFT Aircraft [3] ACI Airports Council International: ACLS Automatic carrier landing system: Aircraft carrier operations ACM Air cycle machine: Part of A/C air conditioning system ACMS Aircraft condition monitoring system ACP Audio Control Panel ACR