Magnus Effect in the Case of Rotating Cylinders and Shell

Magnus Effect in the Case of Rotating Cylinders and Shell PDF Author: William E. Buford
Publisher:
ISBN:
Category : Magnus effect
Languages : en
Pages : 60

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Magnus Effect in the Case of Rotating Cylinders and Shell

Magnus Effect in the Case of Rotating Cylinders and Shell PDF Author: William E. Buford
Publisher:
ISBN:
Category : Magnus effect
Languages : en
Pages : 60

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An Investigation of the Magnus Effect on a Rotating Cylinder

An Investigation of the Magnus Effect on a Rotating Cylinder PDF Author: Palmer Lee Click
Publisher:
ISBN:
Category : Lift (Aerodynamics)
Languages : en
Pages : 74

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860

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WADC Technical Report

WADC Technical Report PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 300

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The Effects of Reynolds Number, Mach Number, Spin Rate, and Other Variables on the Aerodynamics of Spheres at Subsonic and Transonic Velocities

The Effects of Reynolds Number, Mach Number, Spin Rate, and Other Variables on the Aerodynamics of Spheres at Subsonic and Transonic Velocities PDF Author: C. M. Sabin
Publisher:
ISBN:
Category : Sphere
Languages : en
Pages : 32

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 2180

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Paper

Paper PDF Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 870

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Flight Physics

Flight Physics PDF Author: E. Torenbeek
Publisher: Springer Science & Business Media
ISBN: 1402086644
Category : Technology & Engineering
Languages : en
Pages : 540

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Book Description
Knowledge is not merely everything we have come to know, but also ideas we have pondered long enough to know in which way they are related, and 1 how these ideas can be put to practical use. Modern aviation has been made possible as a result of much scienti c - search. However, the very rst useful results of this research became ava- able a considerable length of time after the aviation pioneers had made their rst ights. Apparently, researchers were not able to nd an adequate exp- nation for the occurrence of lift until the beginning of the 21st century. Also, for the fundamentals of stability and control, there was no theory available that the pioneers could rely on. Only after the rst motorized ights had been successfully made did researchers become more interested in the science of aviation, which from then on began to take shape. In modern day life, many millions of passengers are transported every year by air. People in the western societies take to the skies, on average, several times a year. Especially in areas surrounding busy airports, travel by plane has been on the rise since the end of the Second World War. Despite becoming familiar with the sight of a jumbo jet commencing its ight once or twice a day, many nd it astonishing that such a colossus with a mass of several hundred thousands of kilograms can actually lift off from the ground.

Techniques for Measurement of Dynamic Stability Derivatives in Ground Test Facilities

Techniques for Measurement of Dynamic Stability Derivatives in Ground Test Facilities PDF Author: Clarence John Schueler
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 242

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Book Description
Some of the techniques in current use for measuring dynamic stability derivatives in wind tunnels are described, with emphasis given to the important features of balance system design, data reduction methods, instrumentation and typical balance systems. The use of gas bearings for dynamic stability and roll damping balances is treated and a three-degree-of-freedom balance system employing a spherical gas bearing is described. (Author).

Design for Control of Projectile Flight Characteristics

Design for Control of Projectile Flight Characteristics PDF Author: United States. Army Materiel Command
Publisher:
ISBN:
Category : Projectiles, Aerial
Languages : en
Pages : 290

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Book Description
This handbook presents a general survey of the principal factors affecting the flight of projectiles, and describes the methods commonly used for predicting and influencing the flight performance. The coefficients which characterize the aerodynamic forces and moments of a moving body are identified, methods for determining the coefficients applicable to a projectile having a given shape and center of gravity location are described, and the coefficients of a number of projectiles and projectile shapes are given. The use of aerodynamic coefficients in predicting stability, range and accuracy is described. The effects of variations in projectile shape and center of gravity location on range, accuracy and lethality are discussed. Some material on prototype testing and the effects of round-to-round variations in production lots is presented.