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

A feasibility study into the provision of an omni-directional visual glideslope indicator for helicopter off-shore approaches

Smith, A
Civil Aviation Authority, London (United Kingdom)

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:2943.67(CAA-P--95011) / BLDSC - Brit...

A study of the effect of wake passing on turbine blades

Doorly, D.J.

January 1983

SIGLELD:D50632/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Analytical investigation of the effects of blade flexibility, unsteady aerodynamics, and variable inflow on helicopter rotor stall characteristics /

Bellnger, E. D.
United States. National Aeronautics and Space Administration.
United Aircraft Corporation. Research Laboratories.
Langley Research Center.

January 1971

Prepared by United Aircraft Corporation, United Aircraft Research Laboratories, for Langley Research...

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

Trigg, C.J
Royal Air Force Coll., Cranwell (United Kingdom)
Loughborough Univ. of Technology (United Kingdom)

January 1986

In part fulfilment of M.Sc. ThesisAvailable from British Library Document Supply Centre- DSC:6015.42...

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...

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...

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...

Rotor blade flows and ground effect

Purvis, R.

January 2002

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

Experimental investigation of helicopter aerodynamics during quick stop manoeuvres and steep descent

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

January 1995

Final reportSIGLEAvailable from British Library Document Supply Centre- DSC:7620.858(BU-DAE-R--727) ...

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...

Helicopter rotor icing symposium

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

January 1986

Available from British Library Document Supply Centre- DSC:86/17666(Helicopter) / BLDSC - British Li...

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

Markiewicz, R. H.

July 1990

The design of a model helicopter rotor blade incorporating a swept tip is described. The swept tip ...

A study of the aerodynamic characteristics of a propeller and wing including the effect of ground proximity

Harris, A.P

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182209 / BLDSC - British Library D...

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...

A feasibility study into the provision of an omni-directional visual glideslope indicator for helicopter off-shore approaches

Smith, A
Civil Aviation Authority, London (United Kingdom)

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:2943.67(CAA-P--95011) / BLDSC - Brit...

A study of the effect of wake passing on turbine blades

Doorly, D.J.

January 1983

SIGLELD:D50632/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Analytical investigation of the effects of blade flexibility, unsteady aerodynamics, and variable inflow on helicopter rotor stall characteristics /

Bellnger, E. D.
United States. National Aeronautics and Space Administration.
United Aircraft Corporation. Research Laboratories.
Langley Research Center.

January 1971

Prepared by United Aircraft Corporation, United Aircraft Research Laboratories, for Langley Research...

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

Trigg, C.J
Royal Air Force Coll., Cranwell (United Kingdom)
Loughborough Univ. of Technology (United Kingdom)

January 1986

In part fulfilment of M.Sc. ThesisAvailable from British Library Document Supply Centre- DSC:6015.42...

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...

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...

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...

Rotor blade flows and ground effect

Purvis, R.

January 2002

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

Experimental investigation of helicopter aerodynamics during quick stop manoeuvres and steep descent

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

January 1995

Final reportSIGLEAvailable from British Library Document Supply Centre- DSC:7620.858(BU-DAE-R--727) ...

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...

Helicopter rotor icing symposium

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

January 1986

Available from British Library Document Supply Centre- DSC:86/17666(Helicopter) / BLDSC - British Li...

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

Markiewicz, R. H.

July 1990

The design of a model helicopter rotor blade incorporating a swept tip is described. The swept tip ...

A study of the aerodynamic characteristics of a propeller and wing including the effect of ground proximity

Harris, A.P

January 1993

SIGLEAvailable from British Library Document Supply Centre- DSC:DX182209 / BLDSC - British Library D...

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...

A feasibility study into the provision of an omni-directional visual glideslope indicator for helicopter off-shore approaches

Smith, A
Civil Aviation Authority, London (United Kingdom)

January 1995

SIGLEAvailable from British Library Document Supply Centre- DSC:2943.67(CAA-P--95011) / BLDSC - Brit...

A study of the effect of wake passing on turbine blades

Doorly, D.J.

January 1983

SIGLELD:D50632/84 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Analytical investigation of the effects of blade flexibility, unsteady aerodynamics, and variable inflow on helicopter rotor stall characteristics /

Bellnger, E. D.
United States. National Aeronautics and Space Administration.
United Aircraft Corporation. Research Laboratories.
Langley Research Center.

January 1971

Prepared by United Aircraft Corporation, United Aircraft Research Laboratories, for Langley Research...

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

Abstract

Extracted data

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

Abstract

Extracted data

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