Wind tunnel test on a 1/4.622 Froude scale, hingeless rotor, tilt rotor model, volume 2

Development Of The USM Wind Tunnel Validation Model For Calibration

Sim, Chiow Moon

June 2018

Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...

TUNNEL TEST BY

Stephen M. Swanson
Megan S. Mccluer
Gloria K. Yamauchi
Alexandra A. Swanson
Associazione Industrie
I Sistemi E La Difesa
Associazione Italiana
De Aeronautica

January 2015

Blade airloads data were acquired for a 1/4-scale tiltrotor model tested at the Duits-Nederlandse Wi...

Dynamics of vertical axis wind turbines Wind tunnel testing

Courtney, M.S
Done, G.T.S.
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
The City Univ., London (United Kingdom). Dept. of Mechanical Engineering

January 1987

Final report produced Apr 1986SIGLEAvailable from British Library Document Supply Centre- DSC:3816.4...

Wind tunnel tests on thickened and truncated aerofoils for wind turbines

Reddy, M.T
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
Southampton Univ. (United Kingdom). Dept. of Ship Science

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.490(ETSU-WN--5054/1) / BLDSC - ...

Wind-tunnel tests on open-ended building models : final report

Lesher, E. J.

January 1955

http://deepblue.lib.umich.edu/bitstream/2027.42/6266/5/bad5666.0001.001.pdfhttp://deepblue.lib.umich...

High-speed wind tunnel test of the CAE aerodynamic validation model

Roy GEBBINK
Ganglin WANG
Min ZHONG

March 2018

For the purpose of establishing and validating aerodynamic performance predictions at transonic Mach...

Wind Tunnel Measured Effects on a Twin-Engine Short-Haul Transport Caused by Simulated Ice Accretions: Data Report

Ratvasky, Thomas
Potapczuk, Mark
Reehorst, Andrew

May 1997

The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...

Wind tunnel data reduction techniques for aeroelastic models

Upadhya, AR
Ramamurthy, MR
Sundararajan, D

October 1986

Data Reduction technique for Wind tunnel testing of Aeroelastic models with case studies discussed

A survey of transition research at AEDC /

Whitfield, Jack D., author.
Dougherty, N. Sam, author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

This report presents a survey of experimental research on transition Reynolds numbers conducted in a...

An Experimental Evaluation of Wind Tunnel Wall Correction Methods for Helicopter Performance,” 52nd AHS Annual Forum

Hans-juergen Langer
Randall L. Peterson
Thomas H. Maier

January 1996

Accurate measurements of rotorcraft performance as measured in a wind tunnel are strongly influenced...

Wind tunnel tests on a variable camber wing

MacKinnon, A.
Stollery, J
College of Aeronautics, Cranfield (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9304) / BLDSC - Brit...

Wind tunnel tests of two-dimensional and half-axisymmetric inlet models at Mach numbers 1.5 through 3.0 /

Hube, Frederick K., author.
Jenke, Leroy M., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Photocopy.Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.Fi...

Low speed wind tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio

Peckham, D.H
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1987

Report prepared Nov 1968Available from British Library Document Supply Centre- DSC:8717.806(RAE-TR--...

BO 105 flight test data for a wind tunnel test program

Langer, H.J.
Traenapp, N.
Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. (DLR), Braunschweig (Germany). Inst. fuer Flugmechanik

January 1993

The objective of the data correlation is, to find out correction procedures to be applied for rotors...

Wind tunnel test of a non-linear flutter model

Viguier, P.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2003

Communication to : IFASD 2003, Amsterdam (Pays-Bas), June 04-06, 2003SIGLEAvailable from INIST (FR),...

Development Of The USM Wind Tunnel Validation Model For Calibration

Sim, Chiow Moon

June 2018

Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...

TUNNEL TEST BY

Stephen M. Swanson
Megan S. Mccluer
Gloria K. Yamauchi
Alexandra A. Swanson
Associazione Industrie
I Sistemi E La Difesa
Associazione Italiana
De Aeronautica

January 2015

Blade airloads data were acquired for a 1/4-scale tiltrotor model tested at the Duits-Nederlandse Wi...

Dynamics of vertical axis wind turbines Wind tunnel testing

Courtney, M.S
Done, G.T.S.
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
The City Univ., London (United Kingdom). Dept. of Mechanical Engineering

January 1987

Final report produced Apr 1986SIGLEAvailable from British Library Document Supply Centre- DSC:3816.4...

Wind tunnel tests on thickened and truncated aerofoils for wind turbines

Reddy, M.T
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
Southampton Univ. (United Kingdom). Dept. of Ship Science

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:3816.490(ETSU-WN--5054/1) / BLDSC - ...

Wind-tunnel tests on open-ended building models : final report

Lesher, E. J.

January 1955

http://deepblue.lib.umich.edu/bitstream/2027.42/6266/5/bad5666.0001.001.pdfhttp://deepblue.lib.umich...

High-speed wind tunnel test of the CAE aerodynamic validation model

Roy GEBBINK
Ganglin WANG
Min ZHONG

March 2018

For the purpose of establishing and validating aerodynamic performance predictions at transonic Mach...

Wind Tunnel Measured Effects on a Twin-Engine Short-Haul Transport Caused by Simulated Ice Accretions: Data Report

Ratvasky, Thomas
Potapczuk, Mark
Reehorst, Andrew

May 1997

The purpose of this report is to release the data from the NASA Langley/Lewis 14 by 22 foot wind tun...

Wind tunnel data reduction techniques for aeroelastic models

Upadhya, AR
Ramamurthy, MR
Sundararajan, D

October 1986

Data Reduction technique for Wind tunnel testing of Aeroelastic models with case studies discussed

A survey of transition research at AEDC /

Whitfield, Jack D., author.
Dougherty, N. Sam, author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

This report presents a survey of experimental research on transition Reynolds numbers conducted in a...

An Experimental Evaluation of Wind Tunnel Wall Correction Methods for Helicopter Performance,” 52nd AHS Annual Forum

Hans-juergen Langer
Randall L. Peterson
Thomas H. Maier

January 1996

Accurate measurements of rotorcraft performance as measured in a wind tunnel are strongly influenced...

Wind tunnel tests on a variable camber wing

MacKinnon, A.
Stollery, J
College of Aeronautics, Cranfield (United Kingdom)

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(CU-COA--9304) / BLDSC - Brit...

Wind tunnel tests of two-dimensional and half-axisymmetric inlet models at Mach numbers 1.5 through 3.0 /

Hube, Frederick K., author.
Jenke, Leroy M., author.
ARO, Inc., sponsor.
Arnold Engineering Development Center. sponsor.
United States. Air Force. Systems Command. issuing body.

Photocopy.Report was prepared by ARO, Inc., a subsidiary of Sverdrup & Parcel and Associates, Inc.Fi...

Low speed wind tunnel tests of a number of fin configurations on a flat-plate gothic wing of unit aspect ratio

Peckham, D.H
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1987

Report prepared Nov 1968Available from British Library Document Supply Centre- DSC:8717.806(RAE-TR--...

BO 105 flight test data for a wind tunnel test program

Langer, H.J.
Traenapp, N.
Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. (DLR), Braunschweig (Germany). Inst. fuer Flugmechanik

January 1993

The objective of the data correlation is, to find out correction procedures to be applied for rotors...

Wind tunnel test of a non-linear flutter model

Viguier, P.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2003

Communication to : IFASD 2003, Amsterdam (Pays-Bas), June 04-06, 2003SIGLEAvailable from INIST (FR),...

Development Of The USM Wind Tunnel Validation Model For Calibration

Sim, Chiow Moon

June 2018

Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...

TUNNEL TEST BY

Stephen M. Swanson
Megan S. Mccluer
Gloria K. Yamauchi
Alexandra A. Swanson
Associazione Industrie
I Sistemi E La Difesa
Associazione Italiana
De Aeronautica

January 2015

Blade airloads data were acquired for a 1/4-scale tiltrotor model tested at the Duits-Nederlandse Wi...

Dynamics of vertical axis wind turbines Wind tunnel testing

Courtney, M.S
Done, G.T.S.
Energy Technology Support Unit (ETSU), Harwell (United Kingdom)
The City Univ., London (United Kingdom). Dept. of Mechanical Engineering

January 1987

Final report produced Apr 1986SIGLEAvailable from British Library Document Supply Centre- DSC:3816.4...

Wind tunnel test on a 1/4.622 Froude scale, hingeless rotor, tilt rotor model, volume 2

Abstract

Extracted data

Wind tunnel test on a 1/4.622 Froude scale, hingeless rotor, tilt rotor model, volume 2

Abstract

Extracted data

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