New testing capabilities for the supersonic wind tunnel S3MA of the ONERA Modane test centre Roll damping, pitch damping and magnus measurements rigs

High Reynolds number helicopter fuselage test in the ONERA F1 pressurised wind tunnel

Gatard, J.
Costes, M.
Kroll, N. (AND others)
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1997

Communication to : 23rd European rotorcraft forum Dresden (Germany), September 16-18, 1997SIGLEAvail...

Turbine testing at ONERA

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

January 2002

Communication to : 2002 ONERA DLR aerospace symposium, Cologne (Allemagne), June 13-14, 2002SIGLEAva...

Measurement Of Pitch-Damping Derivatives On Prithvi Model In The Nal 1.2m Tunnel

Nagarajan, V
Sundaramurthy, H

August 1990

Pitch Damping Derivatives Were Measured On A 1/12 .5 Scale Prithvi Model Using The Forced Oscillatio...

An updated overview of wind tunnel testing capabilities for civil aircraft development in the large industrial wind tunnels of ONERA

Wolf, S.W.D.
Prieur, J.
Becle, J.P.
Wagner, P.
Quemard, C.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2001

Communication to : CASI 48th annual conference, Toronto (Canada), April 29 - May 02, 2001Available f...

New standard for windtunnel testing technique for propeller driven models at ONERA

Prieur, J.
Sechaud, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2000

Communication to : 21st AIAA advanced measurement technology and ground testing conference, Denver, ...

High Reynolds number air intake tests in the ONERA F1 and S1MA wind-tunnels

Quemard, C.
Raynal, J.-C.
Garcon, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1996

Communication to : Workshop on airframe engine integration at DLR Braunschweig (Germany), March 6-7,...

Wind tunnel testing of propeller driven aircraft models The FLA experience at ONERA

Prieur, J.
Francois, G.
Sechaud, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : 7th european propulsion forum, Pau (France), March 10-12, 1999Available from INIS...

S3MA supersonic test capabilities extension using half nozzles

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

January 1997

Communication to : 87th STA semiannual meeting, Aussois (France), May 4-6, 1997SIGLEAvailable from I...

A new adaptative test section at ONERA Chalais-Meudon

Le Sant, Y.
Bouvier, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1992

Tire de : European Forum on Wind Tunnels and Wind Tunnel Test Techniques, Southampton University (UK...

An overview of supersonic aerodynamics research at ONERA

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

January 2000

Communication to : ECCOMAS 2000, Barcelona (Spain), September 11-14, 2000SIGLEAvailable from INIST (...

Performing high speed tests with ENIFAIR powered nacelles in the S1MA wind-tunnel

Godard, J.L.
Piat, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2000

Communication to : Workshop on European-research on aerodynamic engine / airframe integration for tr...

ONERA activities on supersonic transport aircraft aerodynamics

Thibert, J.J.
Duveau, P.
Grenon, R.
Lemee, P.
Thepot, R.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1998

Communication to : AAAF - ICAS congress, Melbourne (Australia), September 13-18, 1998SIGLEAvailable ...

The 'supersonic aerodynamics' project at ONERA

Arnal, D.
Chanetz, B.
Reneaux, J.
Coustols, E.
Bur, R.
Lewy, S.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2002

Communication to : CEAS aerospace aerodynamics research conference, Cambridge (Grande Bretagne), Jun...

ONERA wind tunnel facilities for reentry vehicle applications

Sagnier, P.
Ledy, J.P.
Chanetz, B.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : AAAF - international symposium atmospheric reentry vehicles and systems, Arcachon...

Improvements on the Control, Data Acquisition and Processing\ud System for the Roll Damping Rig of 1.2m Wind Tunnel

Divya , S
Panneer , Selvan M
Rao, Prasada K

March 2010

The control system was developed to control, acquire and process the data from the specially designe...

High Reynolds number helicopter fuselage test in the ONERA F1 pressurised wind tunnel

Gatard, J.
Costes, M.
Kroll, N. (AND others)
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1997

Communication to : 23rd European rotorcraft forum Dresden (Germany), September 16-18, 1997SIGLEAvail...

Turbine testing at ONERA

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

January 2002

Communication to : 2002 ONERA DLR aerospace symposium, Cologne (Allemagne), June 13-14, 2002SIGLEAva...

Measurement Of Pitch-Damping Derivatives On Prithvi Model In The Nal 1.2m Tunnel

Nagarajan, V
Sundaramurthy, H

August 1990

Pitch Damping Derivatives Were Measured On A 1/12 .5 Scale Prithvi Model Using The Forced Oscillatio...

An updated overview of wind tunnel testing capabilities for civil aircraft development in the large industrial wind tunnels of ONERA

Wolf, S.W.D.
Prieur, J.
Becle, J.P.
Wagner, P.
Quemard, C.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2001

Communication to : CASI 48th annual conference, Toronto (Canada), April 29 - May 02, 2001Available f...

New standard for windtunnel testing technique for propeller driven models at ONERA

Prieur, J.
Sechaud, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2000

Communication to : 21st AIAA advanced measurement technology and ground testing conference, Denver, ...

High Reynolds number air intake tests in the ONERA F1 and S1MA wind-tunnels

Quemard, C.
Raynal, J.-C.
Garcon, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1996

Communication to : Workshop on airframe engine integration at DLR Braunschweig (Germany), March 6-7,...

Wind tunnel testing of propeller driven aircraft models The FLA experience at ONERA

Prieur, J.
Francois, G.
Sechaud, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : 7th european propulsion forum, Pau (France), March 10-12, 1999Available from INIS...

S3MA supersonic test capabilities extension using half nozzles

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

January 1997

Communication to : 87th STA semiannual meeting, Aussois (France), May 4-6, 1997SIGLEAvailable from I...

A new adaptative test section at ONERA Chalais-Meudon

Le Sant, Y.
Bouvier, F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1992

Tire de : European Forum on Wind Tunnels and Wind Tunnel Test Techniques, Southampton University (UK...

An overview of supersonic aerodynamics research at ONERA

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

January 2000

Communication to : ECCOMAS 2000, Barcelona (Spain), September 11-14, 2000SIGLEAvailable from INIST (...

Performing high speed tests with ENIFAIR powered nacelles in the S1MA wind-tunnel

Godard, J.L.
Piat, J.F.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2000

Communication to : Workshop on European-research on aerodynamic engine / airframe integration for tr...

ONERA activities on supersonic transport aircraft aerodynamics

Thibert, J.J.
Duveau, P.
Grenon, R.
Lemee, P.
Thepot, R.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1998

Communication to : AAAF - ICAS congress, Melbourne (Australia), September 13-18, 1998SIGLEAvailable ...

The 'supersonic aerodynamics' project at ONERA

Arnal, D.
Chanetz, B.
Reneaux, J.
Coustols, E.
Bur, R.
Lewy, S.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 2002

Communication to : CEAS aerospace aerodynamics research conference, Cambridge (Grande Bretagne), Jun...

ONERA wind tunnel facilities for reentry vehicle applications

Sagnier, P.
Ledy, J.P.
Chanetz, B.
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1999

Communication to : AAAF - international symposium atmospheric reentry vehicles and systems, Arcachon...

Improvements on the Control, Data Acquisition and Processing\ud System for the Roll Damping Rig of 1.2m Wind Tunnel

Divya , S
Panneer , Selvan M
Rao, Prasada K

March 2010

The control system was developed to control, acquire and process the data from the specially designe...

High Reynolds number helicopter fuselage test in the ONERA F1 pressurised wind tunnel

Gatard, J.
Costes, M.
Kroll, N. (AND others)
Office National d'Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

January 1997

Communication to : 23rd European rotorcraft forum Dresden (Germany), September 16-18, 1997SIGLEAvail...

Turbine testing at ONERA

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

January 2002

Communication to : 2002 ONERA DLR aerospace symposium, Cologne (Allemagne), June 13-14, 2002SIGLEAva...

Measurement Of Pitch-Damping Derivatives On Prithvi Model In The Nal 1.2m Tunnel

Nagarajan, V
Sundaramurthy, H

August 1990

Pitch Damping Derivatives Were Measured On A 1/12 .5 Scale Prithvi Model Using The Forced Oscillatio...

New testing capabilities for the supersonic wind tunnel S3MA of the ONERA Modane test centre Roll damping, pitch damping and magnus measurements rigs

Abstract

Extracted data

New testing capabilities for the supersonic wind tunnel S3MA of the ONERA Modane test centre Roll damping, pitch damping and magnus measurements rigs

Abstract

Extracted data

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