NACA duct

Source: Wikipedia, the free encyclopedia.

Concept picture of a submerged inlet for a jet aircraft

A NACA duct,

air inlet design, originally developed by the U.S. National Advisory Committee for Aeronautics (NACA), the precursor to NASA, in 1945.[2][3]

Design

Prior submerged inlet experiments showed poor

that can occur with protruding scoop designs.

Aircraft applications

Three intakes (facing right) on an engine cowling

When properly implemented, a NACA duct allows air to flow into an internal duct, often for cooling purposes, with a minimal disturbance to the flow. The design was originally called a submerged inlet, since it consists of a shallow ramp with curved walls recessed into the exposed surface of a streamlined body, such as an aircraft.

This type of flush inlet generally cannot achieve the greater ram pressures and flow volumes of an external design, and so is rarely used for the jet engine intake application for which it was originally designed, such as the North American YF-93 and Short SB.4 Sherpa. It is commonly used for piston engine and ventilation intakes.

Automobile applications

The Ferrari F40 sports car has "NACA style" side and hood scoops.

It is especially favored in

Nissan S130. It is also prevalent in some motorcycle designs, such as the 1994–1997 Honda VFR750F or the 1994-1998 Ducati 916
.

See also

References

  1. ^ Frick, Charles W., et al. NACA ACR No. 5120, An Experimental Investigation of NACA Submerged- Duct Entrances. NACA, November 13, 1945. Abstract, Full report.
  2. ^ "NACA UK Mirror report description page".
  3. ^ "MAGiC NACA Archive".
  4. ^ "Duct Soup – How A NACA Duct Works". Hot Rod. 18 July 2013.
  5. . (Practical guidance on designing and building NACA ducts for motor-racing applications)

Further reading