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Index I-9<br />

Pressure force, 40<br />

Pressure gradient, 41<br />

adverse, 300, 490<br />

effect on boundary layer, 488<br />

favorable, 490<br />

Pressure head, 43, 103, 124<br />

Pressure at a jet exit, 110<br />

Pressure prism, 63<br />

Pressure recovery coefficient, 421<br />

Pressure tap, 109<br />

Pressure transducer, 55<br />

strain gage, 56<br />

Primary quantities, 4<br />

Product of inertia, 59<br />

of common areas, 60<br />

Profile, velocity, see Velocity profile<br />

Propeller pump, 671<br />

Properties:<br />

of air, 717, 718<br />

of common gases, 14, 714<br />

of common liquids, 12, 714<br />

of U.S. Standard Atmosphere, 47, 719, 720<br />

of water, 716<br />

Prototype, 354<br />

Pump, 645<br />

affinity laws, 669<br />

axial-flow, 671<br />

blades, 653<br />

centrifugal, 653<br />

dimensionless parameters, 666<br />

double-stage, 654<br />

efficiency, 239<br />

fan, 673<br />

geometrically similar, 666<br />

head, 656, 662<br />

mixed-flow, 671<br />

multistage, 654<br />

parallel, 665<br />

performance curve, 658<br />

propeller, 671<br />

scaling laws, 667, 668<br />

selection, 662<br />

series, 665<br />

similarity laws, 666<br />

single-stage, 654<br />

specific speed, 669<br />

stage, 671<br />

system equation, 662<br />

Quasi-steady flow, 130<br />

Radial-flow machine, 647<br />

Rankine oval, 298<br />

Rapidly varied flow, 536, 555, video V10.9,<br />

video V10.10<br />

Rate of angular deformation, 269, video V6.3<br />

Rate of heat transfer, 223<br />

Rate of shearing strain, 15, 269<br />

Rayleigh, Lord, 29<br />

Rayleigh line flow, 609, 620<br />

basic equations for, 620<br />

graph for calculation of, 723<br />

normal shock in, 624<br />

T–s diagram, 621, 624<br />

Rayleigh Pitot tube formula, 632<br />

Reaction turbine, 673, 682<br />

Rectangular weir, 122, 562<br />

Reentrant entrance, 417<br />

Reference dimensions, 335, 342<br />

Relative roughness, 411, 487<br />

Relative velocity, 176, 196, 218, 647<br />

Repeating variable, 336<br />

Restricted homogeneous equation, 5<br />

Reversible process, 131<br />

Reynolds, O., 29, 348, 385<br />

Reynolds number, 18, 347, 348, 372<br />

critical, see Transition to turbulence<br />

properties of flows with low, 467, 469,<br />

video V1.2, video V7.3, video V7.7, video V9.10<br />

properties of flows with large, 467, 469,<br />

video V1.1, video V7.3<br />

Reynolds pipe flow experiment, 385, video V8.2<br />

Reynolds stress, 404<br />

Reynolds transport theorem, 166, 168, 170, 173<br />

Rheology, 3<br />

Right-hand rule, 218<br />

Rigid body motion of <strong>fluid</strong>, 72<br />

Ripple tank, 634<br />

Rising head curve, 659<br />

Rotameter, 445, video V8.13<br />

Rotation, 130, 264, 267<br />

vector, 268<br />

Rotor, turbomachine, 217, 221, 647, 687<br />

Roughness:<br />

effect on models, 360, 367, video V7.13<br />

on flat plates, 487<br />

in open channels, 549<br />

in pipes, 410<br />

relative, 411<br />

typical values of, 412<br />

Roughness coefficient, Manning, 549<br />

Round-off error, 703<br />

Scale:<br />

length, 358<br />

model, 358<br />

Scaling laws for pumps, 667<br />

Secondary flow:<br />

in a pipe, 421<br />

Secondary quantities, 4<br />

Second law of thermodynamics, 239<br />

Second moment of area, 59<br />

of common areas, 60<br />

Semi-infinitesimal control volume, 239<br />

Separation: video V6.8, video V9.6, video V9.11,<br />

video V9.13<br />

in a boundary layer, 282, 468, 490<br />

in a pipe, 417, 421<br />

with a shock wave, 631<br />

Separation location, 468<br />

on an airfoil, 492<br />

on a cylinder, 468, 490<br />

definition, 490<br />

Shaft:<br />

head, 233<br />

power, 219, 652<br />

torque, 219, 652<br />

work, 219, 652

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