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Relative Roughness, Circular Ducts
标准号:
AIR1168/1
标准名称:
同源图形
Incompressible Flow,
(1A-3)
Boundary Layers and
Pipe Velocity and Fr
(1A-7)
Friction Factor Vers
ReynodlsNumebrinGase
ReynoldsNumberinLqiu
Friction Factor Vers
Bend Loss
Loss Coefficient Ver
Correction Factor fo
Loss Coefficient for
Loss Coefficient for
Loss Coefficient for
Loss Coefficient for
Loss Coefficient Ver
Correction Factor fo
Loss Coefficient for
Loss Coefficient for
Loss Coefficient for
Loss Coefficient for
Effect of Exit Duct
Correction Factor fo
Loss Coefficient for
Loss Coefficient for
Loss Coefficient for
Turning Vanes Geomet
Number of Vanes for
Angle of Attack for
Thin Vanes, Noncircu
Bend Angle and Gap t
Thick Vanes (Calcula
Loss Coefficient for
Effect of Gap to Cho
Loss Coefficient for
Loss Coefficient for
Sketch of Inside and
Pressure Loss Correc
Sketch of Typical Ty
Loss Coefficient of
Loss Coefficient of
Sketch of a Typical
Total Loss Coefficie
Sketch of a Straight
Sketch of a Straight
Curved Wall Diffiise
Sketch of a Truncate
Diffiiser Expansion
Sketch of a Diffuser
Equivalent Expansion
Expansion Factor for
Sketch of an Orifice
Loss Coefficient for
Loss Coefficient for
Contraction Coeffici
Approximate Pressure
Diverging Branch, Fu
Converging Branch, F
Sketch of a Typical
Loss Coefficients, G
Loss Coefficient, Bu
Loss Coefficients fo
Sketch of Heat Excha
Effect of Angle on H
Example of a Duct Sy
Nonflow Work, Compre
Steady-FIow Compress
T-S Diagram
Camot Cycle
Brayton Cycle
Rankine Vapor Cycle
Vapor Cycle in Refri
CompesrisbliiytFacto
Solid and Liquid Pha
Temperature Ratio as
Velocity-Tem peratur
Pressure Ratio as a
Weight Flow Param et
W eight Flow Param e
Flow in a Duct
(1B-84)
Control Volume
Mach Number Function
Control Volume
Friction Factor in D
Effect of W all Fric
Mach Wave Formation
Infinitesim al Flow
Expansion Fan
Prandtl-M eyer Funct
Notation for Normal
Oblique Shock Diagra
Geometric Properties
Effects of Diffuser
Types and Locations
Characteristics of A
Pressure Recovery in
Mass Flow in Turbule
Comparison of NACA D
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Allowable Airframe A
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