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Source: The Open Library

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1Improved method for prediction of attainable wing leading-edge thrust

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“Improved method for prediction of attainable wing leading-edge thrust” Metadata:

  • Title: ➤  Improved method for prediction of attainable wing leading-edge thrust
  • Author:
  • Number of Pages: Median: 60
  • Publisher: Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va

“Improved method for prediction of attainable wing leading-edge thrust” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1996
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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Leading-edge extension

A leading-edge extension (LEX) is a small extension to an aircraft wing surface, forward of the leading edge. The primary reason for adding an extension

Leading edge

one or more of the following: Leading edge boots Leading edge cuffs Leading edge extensions Leading edge slats Leading edge slots Krueger flaps Stall strips

Leading-edge slat

A slat is an aerodynamic surface on the leading edge of the wing of a fixed-wing aircraft. When retracted, the slat lies flush with the rest of the wing

Leading-edge slot

A leading-edge slot is a fixed aerodynamic feature of the wing of some aircraft to reduce the stall speed and promote good low-speed handling qualities

Flap (aeronautics)

where the airflow becomes transonic at high speeds. Thrust gates, or gaps, in the trailing edge flaps may be required to minimise interference between

Thrust reversal

Thrust reversal, also called reverse thrust, is an operating mode for jet engines equipped with a thrust reverser when thrust is directed forwards for

Leading-edge cuff

leading-edge cuff is a wing leading-edge modification, usually a lightly drooped outboard leading-edge extension. In most cases of outboard leading-edge

Leading-edge droop flap

The leading-edge droop flap is a device on the leading edge of aircraft wings designed to improve airflow at high angles of attack. The droop flap is

Krueger flap

may be fitted to the leading edge of an aircraft wing. Unlike slats or droop flaps, the main wing upper surface and its leading edge is not changed. Instead

Inlet cone

that required then the pressure recovery is lower which reduces engine thrust. An inlet with cone may be used to supply high pressure air for ramjet equipment