“Doing good, feeling good? The roles of helping motivation and citizenship pressure”: Correction to Lin, Savani, and Ilies (2019).

2019 ◽  
Vol 104 (11) ◽  
pp. 1433-1433
Keyword(s):  
Pressure Correction ◽  
Good Feeling

Bullying: A ‘No Good’ Feeling on Both Sides

2009 ◽  
Vol 43 (1) ◽  
pp. 15 ◽  
Author(s):  
MICHELE G. SULLIVAN
Keyword(s):  
Good Feeling

“A Gift of Good Feeling”

The Family ◽  
1921 ◽  
Vol 1 (10) ◽  
pp. 13-13
Author(s):  
Mary Blank
Keyword(s):  
Good Feeling

scholarly journals Stability of a Crank-Nicolson pressure correction scheme based on staggered discretizations

2013 ◽  
Vol 74 (1) ◽  
pp. 34-58
Author(s):  
F. Boyer ◽  
F. Dardalhon ◽  
C. Lapuerta ◽  
J.-C. Latché
Keyword(s):  
Pressure Correction ◽  
Correction Scheme ◽  
Crank Nicolson

A Combined Temperature and Pressure Correction Meter

1955 ◽  
Vol 28 (333) ◽  
pp. 516-516 ◽  
Author(s):  
W. S. Lowry ◽  
F. T. Farmer
Keyword(s):  
Pressure Correction ◽  
Temperature And Pressure

scholarly journals Modeling of Tip Clearance Flows Through an Improved 3-D Pressure Correction Navier-Stokes Solver

1993 ◽  
Author(s):  
N. Lymberopoulos ◽  
K. Giannakoglou ◽  
I. Nikolaou ◽  
K. D. Papailiou ◽  
A. Tourlidakis ◽  
...  
Keyword(s):  
Stokes Equations ◽  
Numerical Study ◽  
Three Dimensional ◽  
Tip Clearance ◽  
Navier Stokes ◽  
Special Treatment ◽  
Pressure Correction ◽  
Compressor Rotor ◽  
Numerical Predictions ◽  
Correction Technique

Mechanical constraints dictate the existence of tip clearances in rotating cascades, resulting to a flow leakage through this clearance which considerably influences the efficiency and range of operation of the machine. Three-dimensional Navier-Stokes solvers are often used for the numerical study of compressor and turbine stages with tip-clearance. The quality of numerical predictions depends strongly on how accurately the blade tip region is modelled; in this respect the accurate modelling of tip region was one of the main goals of this work. In the present paper, a 3-D Navier-Stokes solver is suitably adapted so that the flat tip surface of a blade and its sharp edges could be accurately modelled, in order to improve the precision of the calculation in the tip region. The adapted code solves the fully elliptic, steady, Navier-Stokes equations through a space-marching algorithm and a pressure correction technique; the H-type topology is retained, even in cases with thick leading edges where a special treatment is introduced herein. The analysis is applied to two different cases, a linear cascade and a compressor rotor, and comparisons with experimental data are provided.

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