A review of the performance of swept tip helicopters main rotor blades and an analysis of aeroacoustical effects

The HELINOISE Aeroacoustic Rotor Test in the DNW

Splettstoesser, W.R.
Schultz, K.-J.
Junker, B.
Wagner, W.
Weitemeier, B.
Protopsaltis, D.
Fertis, D..

January 1993

In a major cooperative research program between 8 European partners, a geometrically and dynamically...

Experimental results of the European HELINOISE aeroacoustic rotor test in the DNW

Niesl, G. (Eurocopter Deutschland GmbH, Ottobrunn (Germany))
Splettstoesser, W.R. (Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. (DLR), Braunschweig (Germany))
Papanikas, D.G. (ALFAPI, Athens (Greece))
Cenedese, F. (Agusta SpA, Milan (Italy))
Nitti, F. (CIRA SpA, Capua (Italy))
Deutsche Aerospace AG (Dasa), Muenchen (Germany)

January 1993

In a major cooperative research program between 8 European partners, a 40%-geometrically and dynamic...

Helicopter flight control research A demanding application of piloted simulation

Buckingham, S.L
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1986

Paper at RAS Int. Conf. on Flight Simulation of Helicopters - Status and Prospects London (GB) Apr 1...

A study of the aeroelastic behaviour of helicopter rotor blades featuring swept tips

Markiewicz, R
Cranfield Inst. of Tech. (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX93762 / BLDSC - British Library Do...

A review of published literature on helicopter rotor dynamic inflow

Ellenrieder, T
Bristol Univ. (United Kingdom). Dept. of Aerospace Engineering

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:7620.858(BU-DAE--461) / BLDSC - Brit...

Helicopter vibration and its reduction

Royal Aeronautical Society (RAeS), London (United Kingdom)

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:88/07096(Helicopter) / BLDSC - Briti...

A study of the use of blocking masses in reducing helicopter cabin noise

Ellen, C
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1980

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.20(RAE-TM-AERO--1838) / BLDSC -...

An investigation into the phenomenon of helicopter blade sailing

Newman, S.J

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186930 / BLDSC - British Library D...

Rotor blade flows and ground effect

Purvis, R.

January 2002

Available from British Library Document Supply Centre-DSC:DXN053367 / BLDSC - British Library Docume...

Helicopter crashworthiness Study I a review of military and world civil helicopter water impacts over the period 1971-1992; study II an analysis of the response of helicopter structures to water impact

Clifford, W
Civil Aviation Authority, London (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:2943.67(CAA-P--96005) / BLDSC - Briti...

Design and preliminary tests of a blade tip air mass injection system for vortex modification and possible noise reduction on a full-scale helicopter rotor /

Pegg, Robert J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Report of the review of helicopter offshore safety and survival

Civil Aviation Authority, London (United Kingdom)

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:3269.43V(CAA-CAP--641) / BLDSC - Bri...

Investigation and review of helicopter accidents involving surface collision

Bowhay, D.
Ingram, D.
Martin, C.
Civil Aviation Authority, London (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:2943.670(97004 vol 1) / BLDSC - Briti...

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...

A design study for a compound helicopter featured with a convertible prop/rotor

Mostafa, A
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX78468 / BLDSC - British Library Do...

The HELINOISE Aeroacoustic Rotor Test in the DNW

Splettstoesser, W.R.
Schultz, K.-J.
Junker, B.
Wagner, W.
Weitemeier, B.
Protopsaltis, D.
Fertis, D..

January 1993

In a major cooperative research program between 8 European partners, a geometrically and dynamically...

Experimental results of the European HELINOISE aeroacoustic rotor test in the DNW

Niesl, G. (Eurocopter Deutschland GmbH, Ottobrunn (Germany))
Splettstoesser, W.R. (Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. (DLR), Braunschweig (Germany))
Papanikas, D.G. (ALFAPI, Athens (Greece))
Cenedese, F. (Agusta SpA, Milan (Italy))
Nitti, F. (CIRA SpA, Capua (Italy))
Deutsche Aerospace AG (Dasa), Muenchen (Germany)

January 1993

In a major cooperative research program between 8 European partners, a 40%-geometrically and dynamic...

Helicopter flight control research A demanding application of piloted simulation

Buckingham, S.L
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1986

Paper at RAS Int. Conf. on Flight Simulation of Helicopters - Status and Prospects London (GB) Apr 1...

A study of the aeroelastic behaviour of helicopter rotor blades featuring swept tips

Markiewicz, R
Cranfield Inst. of Tech. (United Kingdom)

January 1990

SIGLEAvailable from British Library Document Supply Centre- DSC:DX93762 / BLDSC - British Library Do...

A review of published literature on helicopter rotor dynamic inflow

Ellenrieder, T
Bristol Univ. (United Kingdom). Dept. of Aerospace Engineering

January 1992

SIGLEAvailable from British Library Document Supply Centre- DSC:7620.858(BU-DAE--461) / BLDSC - Brit...

Helicopter vibration and its reduction

Royal Aeronautical Society (RAeS), London (United Kingdom)

January 1987

SIGLEAvailable from British Library Document Supply Centre- DSC:88/07096(Helicopter) / BLDSC - Briti...

A study of the use of blocking masses in reducing helicopter cabin noise

Ellen, C
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1980

SIGLEAvailable from British Library Document Supply Centre- DSC:8670.20(RAE-TM-AERO--1838) / BLDSC -...

An investigation into the phenomenon of helicopter blade sailing

Newman, S.J

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:DX186930 / BLDSC - British Library D...

Rotor blade flows and ground effect

Purvis, R.

January 2002

Available from British Library Document Supply Centre-DSC:DXN053367 / BLDSC - British Library Docume...

Helicopter crashworthiness Study I a review of military and world civil helicopter water impacts over the period 1971-1992; study II an analysis of the response of helicopter structures to water impact

Clifford, W
Civil Aviation Authority, London (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:2943.67(CAA-P--96005) / BLDSC - Briti...

Design and preliminary tests of a blade tip air mass injection system for vortex modification and possible noise reduction on a full-scale helicopter rotor /

Pegg, Robert J.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Report of the review of helicopter offshore safety and survival

Civil Aviation Authority, London (United Kingdom)

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:3269.43V(CAA-CAP--641) / BLDSC - Bri...

Investigation and review of helicopter accidents involving surface collision

Bowhay, D.
Ingram, D.
Martin, C.
Civil Aviation Authority, London (United Kingdom)

January 1997

SIGLEAvailable from British Library Document Supply Centre-DSC:2943.670(97004 vol 1) / BLDSC - Briti...

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...

A design study for a compound helicopter featured with a convertible prop/rotor

Mostafa, A
Cranfield Inst. of Tech. (United Kingdom)

January 1989

SIGLEAvailable from British Library Document Supply Centre- DSC:DX78468 / BLDSC - British Library Do...

The HELINOISE Aeroacoustic Rotor Test in the DNW

Splettstoesser, W.R.
Schultz, K.-J.
Junker, B.
Wagner, W.
Weitemeier, B.
Protopsaltis, D.
Fertis, D..

January 1993

In a major cooperative research program between 8 European partners, a geometrically and dynamically...

Experimental results of the European HELINOISE aeroacoustic rotor test in the DNW

Niesl, G. (Eurocopter Deutschland GmbH, Ottobrunn (Germany))
Splettstoesser, W.R. (Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. (DLR), Braunschweig (Germany))
Papanikas, D.G. (ALFAPI, Athens (Greece))
Cenedese, F. (Agusta SpA, Milan (Italy))
Nitti, F. (CIRA SpA, Capua (Italy))
Deutsche Aerospace AG (Dasa), Muenchen (Germany)

January 1993

In a major cooperative research program between 8 European partners, a 40%-geometrically and dynamic...

Helicopter flight control research A demanding application of piloted simulation

Buckingham, S.L
Royal Aircraft Establishment (RAE), Farnborough (United Kingdom)

January 1986

Paper at RAS Int. Conf. on Flight Simulation of Helicopters - Status and Prospects London (GB) Apr 1...

A review of the performance of swept tip helicopters main rotor blades and an analysis of aeroacoustical effects

Abstract

Extracted data

A review of the performance of swept tip helicopters main rotor blades and an analysis of aeroacoustical effects

Abstract

Extracted data

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