Andere Kunden interessierten sich auch für
![The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles]( "The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles")
The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles63,99 €![Aerodynamic Shape Optimization Using Control Theory]( "Aerodynamic Shape Optimization Using Control Theory")
Aerodynamic Shape Optimization Using Control Theory63,99 €![Optimal Spacecraft Attitude Controlusing Aerodynamic Torques]( "Optimal Spacecraft Attitude Controlusing Aerodynamic Torques")
Optimal Spacecraft Attitude Controlusing Aerodynamic Torques63,99 €![Two Prize Essays On The Characteristics And Advantages Of Literary And Scientific Institutions]( "Two Prize Essays On The Characteristics And Advantages Of Literary And Scientific Institutions")
Two Prize Essays On The Characteristics And Advantages Of Literary And Scientific Institutions25,99 €![Is Your Stratagem Showing? the U.S. Lack of Understanding Chinese Characteristics in Information Warfare]( "Is Your Stratagem Showing? the U.S. Lack of Understanding Chinese Characteristics in Information Warfare")
Is Your Stratagem Showing? the U.S. Lack of Understanding Chinese Characteristics in Information Warfare63,99 €![New Media Analysis: The Effects of Peer Influence and Personality Characteristics through the Stages of Trial, Adoption, and Continued Use]( "New Media Analysis: The Effects of Peer Influence and Personality Characteristics through the Stages of Trial, Adoption, and Continued Use")
New Media Analysis: The Effects of Peer Influence and Personality Characteristics through the Stages of Trial, Adoption, and Continued Use63,99 €![Calculation of the Actual Cost of Engine Maintenance]( "Calculation of the Actual Cost of Engine Maintenance")
Calculation of the Actual Cost of Engine Maintenance63,99 €
The basic objective of this thesis is to provide a practical method of computing the aerodynamic characteristics of slender finned vehicles such as sounding rockets, high speed bombs, and guided missiles. The aerodynamic characteristics considered are the normal force coefficient derivative, c(sub N(sub alpha)); center of pressure, bar-X; roll forcing moment coefficient derivative, c(sub l(sub delta)); roll damping moment coefficient derivative, c(sub l(sub p)); pitch damping moment coefficient derivative, c(sub mq); and the drag coefficient, c (sub D). Equations are determined for both subsonic and supersonic flow. No attempts is made to analyze the transonic region. The general configuration to which the relations are applicable is a slender axisymmetric body having three or four fins.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.