What Makes Airplanes Fly?: History, Science, and Applications of AerodynamicsNew York, 1991 - 225 strán (strany) |
Vyhľadávanie v obsahu knihy
Výsledky 1 - 3 z 72.
Strana 62
... given time - must , of course , remain the same at any cross - sectional area in the tube . It is computed from the product of flow speed and area ; with the dimensions of A ( L2 ) and u ( L / T ) , this product yields Q ( L3 / T ) . We ...
... given time - must , of course , remain the same at any cross - sectional area in the tube . It is computed from the product of flow speed and area ; with the dimensions of A ( L2 ) and u ( L / T ) , this product yields Q ( L3 / T ) . We ...
Strana 102
... given by Newton's law of force : mass of the car times its acceleration . From elementary mechanics ( see , e.g. , Table A2.2 ) , we recall that the work done in this process is given by the force times the distance covered to arrive at ...
... given by Newton's law of force : mass of the car times its acceleration . From elementary mechanics ( see , e.g. , Table A2.2 ) , we recall that the work done in this process is given by the force times the distance covered to arrive at ...
Strana 197
... given by approximately 1.5 x 1011 m [ 150 million km ] , but no specific prefix has been assigned to 1011 , or conversely to 10-11 . ) In Table A3.3 conversion factors are given for quantities in the SI system from the British system ...
... given by approximately 1.5 x 1011 m [ 150 million km ] , but no specific prefix has been assigned to 1011 , or conversely to 10-11 . ) In Table A3.3 conversion factors are given for quantities in the SI system from the British system ...
Obsah
Milestones of the Modern Age | 25 |
The Nature of Liquids and Gases | 41 |
The Atmosphere of the Earth | 47 |
Autorské práva | |
12 zvyšných častí nezobrazených
Iné vydania - Zobraziť všetky
Časté výrazy a frázy
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