What Makes Airplanes Fly?: History, Science, and Applications of AerodynamicsNew York, 1991 - 225 strán (strany) |
Vyhľadávanie v obsahu knihy
Výsledky 1 - 3 z 50.
Strana 42
... dynamic viscosity , μ ( mu ) , kinematic viscosity , v ( nu ) , and their dimensionless ratios with respect to air . In these ratios the subscript i designates the substances listed in the first column . Values apply to p = 1 atm = 14.7 ...
... dynamic viscosity , μ ( mu ) , kinematic viscosity , v ( nu ) , and their dimensionless ratios with respect to air . In these ratios the subscript i designates the substances listed in the first column . Values apply to p = 1 atm = 14.7 ...
Strana 86
... dynamic pressure . This result is obtained if we multiply the coefficients by qS to get the forces . The dependency of the forces on the square of the speed was first described by Isaac Newton in his Prin- cipia , as we mentioned in ...
... dynamic pressure . This result is obtained if we multiply the coefficients by qS to get the forces . The dependency of the forces on the square of the speed was first described by Isaac Newton in his Prin- cipia , as we mentioned in ...
Strana 132
... dynamic equilibrium , given by a number of oscillations about the ultimate stable flight of the arrow . The dynamic adjustment to stable equilibrium is a time - dependent process during which the amplitude of the oscillations- the ...
... dynamic equilibrium , given by a number of oscillations about the ultimate stable flight of the arrow . The dynamic adjustment to stable equilibrium is a time - dependent process during which the amplitude of the oscillations- the ...
Obsah
Milestones of the Modern Age | 25 |
The Nature of Liquids and Gases | 41 |
The Atmosphere of the Earth | 47 |
Autorské práva | |
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aerodynamic drag aeronautics aircraft airfoil airliners airplane airship altitude angle of attack Appendix apply atmosphere automobile aviation balloon Bernoulli's equation birds body boundary layer Cayley Cayley's Chapter computed constant craft cylinder density dimensionless dimensions discussed distance drag and lift drag coefficient effect energy engine experiments fact flight speed flow field flow speed fluid mechanics flying machines fuel gases given gliders increase inviscid jet turbines km/h laminar lift force Lilienthal liquids Mach number Magnus effect mass motion moving ornithopter parameters passengers pilot plane plate pressure problems produced propeller propulsion range ratio Reynolds number rocket shape shear shock wave shown in Figure space speed of sound sphere steady streamlines supersonic surface friction Table temperature test section thrust tion trailing edge transport tube turbojet turbulent boundary layer turn unit values velocity vortex vortices wind tunnel wing Wright brothers Wright Flyer