By Frank Hitchens

The Encyclopedia of Aerodynamics used to be written for pilots in any respect degrees from deepest pilot to airline pilot, army pilots and scholars of aerodynamics as an entire reference handbook to aerodynamic terminology. basic aerodynamic textual content books for pilots are really constrained of their scope whereas aerodynamic textual content books for engineering scholars contain complicated calculus. The references during this booklet, The Encyclopedia of Aerodynamics, are essentially defined and in simple terms easy algebra is utilized in a couple of references yet is totally with out any calculus - a bonus to many readers. Over 1400 references are incorporated with replacement phrases used the place acceptable and cross-referenced all through. The textual content is illustrated with 178 pictures and ninety six diagrams. The Encyclopedia of Aerodynamics is a perfect aerodynamic reference handbook for any pilot’s bookshelf.

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Aircraft-pilot coupling See Pilot induced oscillation (PIO). Aircraft principle axes An aircrafts frame of reference involving the body or geometric axes. See Axes; Body axes. Aircraft wake turbulence See Wingtip vortices. Air density The density of air has a significant effect on aircraft performance and features in the formulas for lift and drag, being part of the dynamic pressure. Air density is determined by air pressure, temperature and the amount of moisture within the air mass. ft and varies with altitude and air temperature.

He is best remembered for his introduction of the blunt nose aerodynamic theory for aerospace vehicles. A blunt nose diffuses much of the heat generated during re-entry to the Earth’s atmosphere. Fellow scientist, Alfred J. Eggers Jr. (1922–2006) assisted him. See Blunt nose re-entry vehicle. All-flying tailplane An all-flying tailplane is one with a variable- incidence – not fixed as on a conventional tailplane/elevator. Allflying tailplanes are more powerful than a conventional tailplane/ elevator system and can produce greater pitching forces.

Airfoil loading The term airfoil loading refers to the pressure distribution over the wing in a chordwise direction (from leading edge to trailing edge). Airfoil nomenclature In the first few years of the 20th Century, many airfoils designs were introduced without any form of classification. However, in the late 1930s, NACA introduced an ordered numbering system to identify and classify the families of airfoils available. Their first method used the four-digit numbering system, which indicates the geometric features of the wing, suitable for low-speed aircraft; this was followed later by the fivedigit series.

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