By Frank Hitchens
The Encyclopedia of Aerodynamics was once written for pilots in any respect degrees from deepest pilot to airline pilot, army pilots and scholars of aerodynamics as a whole reference handbook to aerodynamic terminology. common aerodynamic textual content books for pilots are rather constrained of their scope whereas aerodynamic textual content books for engineering scholars contain advanced calculus. The references during this publication, The Encyclopedia of Aerodynamics, are sincerely defined and merely easy algebra is utilized in a number 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 applicable and cross-referenced all through. The textual content is illustrated with 178 photos and ninety six diagrams. The Encyclopedia of Aerodynamics is a perfect aerodynamic reference guide for any pilot’s bookshelf.
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Extra resources for The Encyclopedia of Aerodynamics
Sample text
The beginnings of aerodynamics can be traced as far back to the time of Daniel Bernoulli (1700–1782) and Leonhard Euler (1707–1783) and others. Many other great names have been involved with the development of aerodynamics especially in the first half of the 20th Century and can be attributed to a select few – the fathers of aerodynamics. The early scientists originally referred to classical aerodynamics as fluid dynamics. Classical aerodynamics is based largely on Newton’s three Laws of Motion taken from Newtonian mechanics and Bernoulli’s Theorem.
Whitcomb (1921–2009) in 1953 discovered the fact that indenting the fuselage at the wing root would reduce shockwave drag at the fuselage/wing junction. He was credited with this discovery, and received the Collier Trophy in 1954 during his work at NASA Langley. Although Richard Whitcomb received the credit for introducing the area rule concept, Dr. Dietrich Küchemann (1911–1976), the German aerodynamicist, had previously addressed the idea. During the 1930–1940s in Germany, he pioneered the area rule concept when studying supersonic airflow problems.
Airfoils are designed to provide an aerodynamic reaction in the form of lift on the wings, or rotor blades and thrust on propellers. Due to the airfoils shape, it produces an aerodynamic reaction (loosely, lift by suction) over the upper surface. Airfoils are further classed as symmetrical or asymmetrical (cambered) airfoils. A symmetrical airfoil has both sides of equal curvature, as found for example on the tail fin. An asymmetrical airfoil (cambered) is found for example on most main wings. Airfoil section A theoretical two-dimensional cross-section of the wing cut along the chord line showing the shape (chord and camber) of the wing.
The Encyclopedia of Aerodynamics by Frank Hitchens
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