Final report on effects of Reynolds number on unsteady flow response of NACA 0020 aerofoil

The collected data for ramp function tests on a NACA 23012 aerofoil Volume 1: desciption and pressure data

Seto, L.Y.
Galbraith, R.A.McD
Glasgow Univ. (United Kingdom). Dept. of Aeronautics and Fluid Mechanics

January 1984

SIGLEAvailable from British Library Lending Division - LD:7620.935(GU--AERO--8413) / BLDSC - British...

The effects of reynolds number on flow separation of Naca Aerofoil

Ab. Wahid, Mastura
Abdul Hakim, Muhammad Syahmi
Dahalan, Md. Nizam
Mansor, Shuhaimi
Wan Ali, Wan Khairuddin
Othman, Norazila
Mat, Shabudin

January 2018

The purpose of this study is to investigate the flow separation above UTM 2D Airfoil at three differ...

NACA Technical Reports

This collection of data on airfoils has been made from the published reports of a number of the lead...

Final report on aerodynamic tests on NACA 0020 aerofoils

Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
University Coll., London (United Kingdom). Dept. of Mechanical Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.49(ETSU-WN--5038/1) / BLDSC - B...

The aerodynamic performance of the NACA-4415 aerofoil section at low Reynolds numbers

Saliveros, E

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186721 / BLDSC - British Library D...

Numerical methods for the design and unsteady analysis of aerofoils

Vezza, M

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:DX81920 / BLDSC - British Library Do...

Reynolds Number Effects on Unsteady Boundary Layer for an Oscillating Airfoil

Dong-ha Kim
Jo-won Chang

January 2016

An experimental study was conducted in order to investigate the influence of Reynolds number on an o...

The design and low Mach number wind-tunnel performance of a modified Naca 23012 aerofoil, with an investigation of dynamic stall onset

Gracey, M.W.

January 1991

SIGLEAvailable from British Library Document Supply Centre-DSC:DX209661 / BLDSC - British Library Do...

Studies of the flow field near a NACA 4412 aerofoil at nearly maximum lift

Williams, B.R
Hastings, R.C.
Royal Aircraft Establishment, Farnborough (United Kingdom)

January 1984

SIGLEAvailable from British Library Lending Division - LD:8670.2(RAE-TM-AERO--2026) / BLDSC - Britis...

Collected Data for Oscillatory Pitch Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data for a Reynolds Number 1.0 Million. G.U. Aero Report 8600

Leishman, J.G.
Seto, L.Y.
Galbraith, R.A.McD.

March 1986

Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...

Collected Data for Oscillatory Pitch Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data for a Reynolds Number 1.0 Million. G.U. Aero Report 8600

Leishman, J.G.
Seto, L.Y.
Galbraith, R.A.McD.

March 1986

Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...

Numerical study of the unsteady aerodynamics of helicopter rotor aerofoils

Shaw, S.T.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN024587 / BLDSC - British Library D...

Influence of Reynolds number on performance of the six airfoils (DU00-W2-401, DU00-W2-350, DU97-W-300, DU91-W2-250, NACA 63421 and NACA 64618).

Mingwei Ge (821186)
Le Fang (328237)
De Tian (821187)

November 2015

(A) the maximum Cl/Cd vs. Re, (B) the co...

NACA Technical Reports

Goett, Harry J
Bullivant, W Kenneth

January 1939

An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...

Solution of the Reynolds-averaged Navier-Stokes equations for transonic aerofoil flows

Johnston, L
University of Manchester Inst. of Science and Technology (UMIST) (United Kingdom). Dept. of Mechanical Engineering

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:9113.125(UMIST-TFD--91/1) / BLDSC - ...

The collected data for ramp function tests on a NACA 23012 aerofoil Volume 1: desciption and pressure data

Seto, L.Y.
Galbraith, R.A.McD
Glasgow Univ. (United Kingdom). Dept. of Aeronautics and Fluid Mechanics

January 1984

SIGLEAvailable from British Library Lending Division - LD:7620.935(GU--AERO--8413) / BLDSC - British...

The effects of reynolds number on flow separation of Naca Aerofoil

Ab. Wahid, Mastura
Abdul Hakim, Muhammad Syahmi
Dahalan, Md. Nizam
Mansor, Shuhaimi
Wan Ali, Wan Khairuddin
Othman, Norazila
Mat, Shabudin

January 2018

The purpose of this study is to investigate the flow separation above UTM 2D Airfoil at three differ...

NACA Technical Reports

This collection of data on airfoils has been made from the published reports of a number of the lead...

Final report on aerodynamic tests on NACA 0020 aerofoils

Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
University Coll., London (United Kingdom). Dept. of Mechanical Engineering

January 1985

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.49(ETSU-WN--5038/1) / BLDSC - B...

The aerodynamic performance of the NACA-4415 aerofoil section at low Reynolds numbers

Saliveros, E

January 1988

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186721 / BLDSC - British Library D...

Numerical methods for the design and unsteady analysis of aerofoils

Vezza, M

January 1986

SIGLEAvailable from British Library Document Supply Centre- DSC:DX81920 / BLDSC - British Library Do...

Reynolds Number Effects on Unsteady Boundary Layer for an Oscillating Airfoil

Dong-ha Kim
Jo-won Chang

January 2016

An experimental study was conducted in order to investigate the influence of Reynolds number on an o...

The design and low Mach number wind-tunnel performance of a modified Naca 23012 aerofoil, with an investigation of dynamic stall onset

Gracey, M.W.

January 1991

SIGLEAvailable from British Library Document Supply Centre-DSC:DX209661 / BLDSC - British Library Do...

Studies of the flow field near a NACA 4412 aerofoil at nearly maximum lift

Williams, B.R
Hastings, R.C.
Royal Aircraft Establishment, Farnborough (United Kingdom)

January 1984

SIGLEAvailable from British Library Lending Division - LD:8670.2(RAE-TM-AERO--2026) / BLDSC - Britis...

Collected Data for Oscillatory Pitch Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data for a Reynolds Number 1.0 Million. G.U. Aero Report 8600

Leishman, J.G.
Seto, L.Y.
Galbraith, R.A.McD.

March 1986

Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...

Collected Data for Oscillatory Pitch Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data for a Reynolds Number 1.0 Million. G.U. Aero Report 8600

Leishman, J.G.
Seto, L.Y.
Galbraith, R.A.McD.

March 1986

Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...

Numerical study of the unsteady aerodynamics of helicopter rotor aerofoils

Shaw, S.T.

January 1999

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN024587 / BLDSC - British Library D...

Influence of Reynolds number on performance of the six airfoils (DU00-W2-401, DU00-W2-350, DU97-W-300, DU91-W2-250, NACA 63421 and NACA 64618).

Mingwei Ge (821186)
Le Fang (328237)
De Tian (821187)

November 2015

(A) the maximum Cl/Cd vs. Re, (B) the co...

NACA Technical Reports

Goett, Harry J
Bullivant, W Kenneth

January 1939

An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...

Solution of the Reynolds-averaged Navier-Stokes equations for transonic aerofoil flows

Johnston, L
University of Manchester Inst. of Science and Technology (UMIST) (United Kingdom). Dept. of Mechanical Engineering

January 1991

SIGLEAvailable from British Library Document Supply Centre- DSC:9113.125(UMIST-TFD--91/1) / BLDSC - ...

The collected data for ramp function tests on a NACA 23012 aerofoil Volume 1: desciption and pressure data

Seto, L.Y.
Galbraith, R.A.McD
Glasgow Univ. (United Kingdom). Dept. of Aeronautics and Fluid Mechanics

January 1984

SIGLEAvailable from British Library Lending Division - LD:7620.935(GU--AERO--8413) / BLDSC - British...

The effects of reynolds number on flow separation of Naca Aerofoil

Ab. Wahid, Mastura
Abdul Hakim, Muhammad Syahmi
Dahalan, Md. Nizam
Mansor, Shuhaimi
Wan Ali, Wan Khairuddin
Othman, Norazila
Mat, Shabudin

January 2018

The purpose of this study is to investigate the flow separation above UTM 2D Airfoil at three differ...

NACA Technical Reports

This collection of data on airfoils has been made from the published reports of a number of the lead...

Final report on effects of Reynolds number on unsteady flow response of NACA 0020 aerofoil

Abstract

Extracted data

Final report on effects of Reynolds number on unsteady flow response of NACA 0020 aerofoil

Abstract

Extracted data

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