Two-phase flow Reynolds number

Two-phase flow Reynolds number, Total:48 items.

The international standard classification for "Two-phase flow Reynolds number" includes: Stationary containers and tanks , Extraction and processing of petroleum and natural gas .

The Chinese standard classification for "Two-phase flow Reynolds number" includes: Pressure vessel , Petroleum development .

General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China

HB 8598-2021 Design requirements for semi-model of aircraft low-speed pressurized wind tunnel high Reynolds number test
HB 8601-2021 Full model design requirements for aircraft low-speed pressurized wind tunnel high Reynolds number tests
HB 8599-2021 Installation requirements for aircraft low-speed pressurized wind tunnel high Reynolds number test model

ASHRAE FUNDAMENTALS IP CH 5-2021 TWO-PHASE FLOW
ASHRAE FUNDAMENTALS SI CH 5-2021 Two-Phase Flow
ASHRAE FUN SI CH 4-2001 Two-Phase Flow(ASHRAE Handbook: Fundamentals, SI Edition)
ASHRAE FUN IP CH 4-2001 Two-Phase Flow(ASHRAE Handbook: Fundamentals, IP Edition)

ESDU 11006-2011 Extrapolating wind-tunnel data to full-scale Reynolds number Part 3: Example (ii) Comparison of extrapolated low-Reynolds-number lift measurements on the F4 wing/body with high-Reynolds-number measurements
ESDU 73017 C-2013 Reynolds number@ speed of sound@ dynamic viscosity@ kinetic pressure and total pressure coefficient in air
ESDU 73017 B-1977 Reynolds number@ speed of sound@ dynamic viscosity@ kinetic pressure and total pressure coefficient in air.
ESDU 07010-2007 Extrapolating wind-tunnel data to full-scale Reynolds number Part 2: Procedures
ESDU 05022-2006 Extrapolating wind-tunnel data to full-scale Reynolds number. Part 1: Principles
FMI2 A-1978 GUIDE TO THE FLOW RELATIONSHIPS AND STATISTICAL METHODS USED IN THE DATA ITEMS ON TWO-PHASE FLOW PRESSURE GRADIENTS IN STRAIGHT PIPES
FMI2 B-2007 Guide to the flow relationships and statistical methods used in the Data Items on two-phase flow pressure gradients in straight pipes.
ESDU 89012-1989 TWO-PHASE FLOW PRESSURE LOSSES IN PIPELINE FITTINGS

NASA NACA-RM-L50K06-1951 Horizontal-tail effectiveness and downwash surveys for two 47.7 degrees sweptback wing-fuselage combinations with aspect ratios of 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
NASA-TM-4363-1992 Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers
NASA-TM-76710-1982 Influence of the Reynolds number on the normal forces of slender bodies of revolution
NASA NACA-TN-2960-1953 Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers
NASA NACA-RM-A52B20-1952 The effects of Reynolds number at Mach numbers up to 0.94 on the loading on a 35 degree swept-back wing having NACA 65(1)A012 streamwise sections
NASA-TR-R-300-1969 Aerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbers
NASA NACA-TN-3963-1957 A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry
NASA NACA-RM-L7E13-1947 Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degrees Sweptback Wing at Reynolds Numbers to 8,000,000

API REPORT 1-1976 Orifice Coefficients for Two-Phase Flow Through Velocity Controlled Subsurface Safety Valves
API OSAPR-1-1976 ORIFICE COEFFICIENTS FOR TWO-PHASE FLOW THROUGH VELOCITY CONTROLLED SUBSURFACE SAFETY VALVES

REG NACA-TN-2463-1951 Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range