Rotary Wings

130 books
Integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades using multilevel decompositionUnknown Author

Integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades using multilevel decomposition

Unknown Author

1995No page data
Helicopter main-rotor noiseThomas F. Brooks
⏱ 1h 2m

Helicopter main-rotor noise

Thomas F. Brooks

198862 pp.
Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flightHarry L. Runyan
⏱ 18m

Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight

Harry L. Runyan

198518 pp.
Application of response surface techniques to helicopter rotor blade optimization procedureJoseph Lynn Henderson

Application of response surface techniques to helicopter rotor blade optimization procedure

Joseph Lynn Henderson

1995No page data
A method to analyze and optimize the load sharing of split path transmissionsT. L. Krantz

A method to analyze and optimize the load sharing of split path transmissions

T. L. Krantz

1997No page data
Rotorcraft system identificationNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 4h 33m

Rotorcraft system identification

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1991273 pp.
Aerodynamics of rotorcraftNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 4h 45m

Aerodynamics of rotorcraft

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990285 pp.
A rigorous framework for optimization of expensive functions by surrogatesUnknown Author

A rigorous framework for optimization of expensive functions by surrogates

Unknown Author

1998No page data
Numerical simulation of helicopter multi-bladed rotor flowC. L. Chen
⏱ 11m

Numerical simulation of helicopter multi-bladed rotor flow

C. L. Chen

198811 pp.
An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor bladesAditi Chattopadhyay
⏱ 14m

An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades

Aditi Chattopadhyay

199014 pp.
Centers of excellence in rotary wing aircraft technologyU.S. Army Research Office
⏱ 1h 6m

Centers of excellence in rotary wing aircraft technology

U.S. Army Research Office

198466 pp.
Recent advances in integrated multidisciplinary optimization of rotorcraftHoward M. Adelman
⏱ 12h 1m

Recent advances in integrated multidisciplinary optimization of rotorcraft

Howard M. Adelman

1993721 pp.
Rotor-fuselage interactionsBarry, John D.

Rotor-fuselage interactions

Barry, John D.

1997No page data
Aeroelastic effects in multirotor vehiclesC. Venkatesan
⏱ 2h 39m

Aeroelastic effects in multirotor vehicles

C. Venkatesan

1987159 pp.
Description of the U.S. Army small-scale 2-meter rotor test systemArthur E. Phelps
⏱ 57m

Description of the U.S. Army small-scale 2-meter rotor test system

Arthur E. Phelps

198757 pp.
A prediction of helicopter rotor discrete frequency noise for three scale models using a new acoustics programKenneth S. Brentner
⏱ 12m

A prediction of helicopter rotor discrete frequency noise for three scale models using a new acoustics program

Kenneth S. Brentner

198712 pp.
The solution of a singular integral equation arising from a lifting surface theory for rotating bladesMark H. Dunn
⏱ 2h 24m

The solution of a singular integral equation arising from a lifting surface theory for rotating blades

Mark H. Dunn

1991144 pp.
Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test programDanny R. Hoad
⏱ 1h 36m

Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test program

Danny R. Hoad

198696 pp.
Representation of a lifting line in an arbitrary motion by a line of acceleration doubletsRoland Dat
⏱ 18m

Representation of a lifting line in an arbitrary motion by a line of acceleration doublets

Roland Dat

197018 pp.
Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the bladeT. A. Millott
⏱ 6h 38m

Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade

T. A. Millott

1994398 pp.
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