Rotors (Helicopters) -- Aerodynamics
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The concept Rotors (Helicopters) -- Aerodynamics represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
The Resource
Rotors (Helicopters) -- Aerodynamics
Resource Information
The concept Rotors (Helicopters) -- Aerodynamics represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Rotors (Helicopters) -- Aerodynamics
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- (EG-IN)628553
72 Items that share the Concept Rotors (Helicopters) -- Aerodynamics
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- Wind-tunnel evaluation of an aeroelastically conformable rotor
- A full potential flow analysis with realistic wake influence for helicopter rotor airload prediction
- Acoustic characteristics of 1/20-scale model helicopter rotors
- Advanced rotor actuation concepts
- Advancing Blade Concept (ABC) technology demonstrator
- Aeorelastic analysis for helicopter rotor blades with time-variable, nonlinear structural twist and multiple structural redundancy-mathematical derivation and program user's manual
- Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade
- Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
- Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets
- Aeroelastic effects in multi-rotor vehicles with application to a hybrid heavy lift system
- Airframe, wing, and tail aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed
- An analysis of the gust-inducesd overspeed trends of helicopter rotors
- An analysis of three-dimensional transonic compressors
- An experimental investigation of the parallel blade-vortex interaction
- Bearingless tail rotor loads and stability
- Calculation of three-dimensional unsteady transonic flows past helicopter blades
- Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
- Computation of rotor aerodynamic loads in forward flight using a full-span free wake analysis
- Computational analysis of high resolution unsteady airloads for rotor aeroacoustics
- Cooperative agreement #NCC 2-175 entitled Investigation of a free-tip rotor configuration for research on spanwise life distributions and wake velocity surveys of a semi-span wing with a discontinuous twist : final report
- Correlation of puma airloads : evaluation of CFD prediction methods
- Development and application of an analysis of axisymmetric body effects on helicopter rotor aerodynamics using modified slender body theory
- Development and validation of a combined rotor-fuselage induced flow-field computational method
- Dynamic system coupling (DYSCO) program
- Effect of blade planform variation on the forward-flight performance of small-scale rotors
- Effect of primary rotor parameters on flapping dynamics
- Effect of rotor wake on aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft
- Estimation of blade airloads from rotor blade bending moments
- Euler equation computations for the flow over a hovering helicopter rotor
- Evaluation of lightweight, composite, impact-resistant tail rotor drive shafting for helicopters
- Evaluation of pylon focusing for reduced helicopter vibration
- Final report on advanced adaptive computational methods for Navier-Stokes simulations in rotorcraft aerodynamics
- Flapping inertia for selected rotor blades
- Fundamentals of fixed and rotary wing aerodynamics
- Growian rotor blades : production development, construction and test
- Helicopter blade dynamic loads measured during performance testing of two scaled rotors
- Helicopter flow field analysis
- Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight, Volume 1, Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec
- Interactional aerodynamics of the single rotor helicopter configuration
- Investigation of helicopter rotor blade/wake interactive impulsive noise
- Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight
- Investigation of the compliant rotor concept
- Load and stability measurements on a soft-inplane rotor system incorporating elastomeric lead-lag dampers
- Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
- MM&T--low cost production/installation of urethane leading edge guards on rotor blades
- Noise of a model helicopter rotor due to ingestion of turbulence
- Numerical analysis of the first static calibration of the RSRA helicopter active-isolator rotor balance system
- Optimization methods applied to the aerodynamic design of helicopter rotor blades
- Performance testing of a main rotor system for a utility helicopter at 1/4 scale
- Preliminary design study of a higher harmonic blade feathering control system
- RWF rotor-wake-fuselage code software reference guide
- Reconstruction of a three-dimensional transonic rotor flow field from holographic interferogram data
- Rotary-wing aerodynamics
- Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program
- Rotorcraft flight simulation computer program C81 with DATAMAP interface
- Rotorcraft flight-propulsion control integration : an eclectic design concept
- Studies in a transonic rotor aerodynamics and noise facility
- Studies of a flat wake rotor theory
- Synthesis of individual rotor blade control system for gust alleviation : final report
- Tail contribution to the directional aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with a tail rotor
- The calculation of rotor/fuselage interaction for two-dimensional bodies
- The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
- The vibration characteristics of a coupled helicopter rotor-fuselage by a finite element analysis
- Thermal analysis of a planetary transmission with spherical roller bearings operating after complete loss of oil
- Tilt rotor hover aeroacoustics
- Transonic flow analysis for rotors
- Transonic rotor tip design using numerical optimization
- UH-60A Black Hawk engineering simulation program
- Wake geometry effects on rotor blade-vortex interaction noise directivity
- Wind tunnel test of a variable-diameter tiltrotor (VDTR) model
- Wind tunnel tests of large and small scale rotor hubs and pylons
- Wind-tunnel evaluation of an advanced main-rotor blade design for a utility-class helicopter
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/a2u22cX-ofo/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/a2u22cX-ofo/">Rotors (Helicopters) -- Aerodynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/a2u22cX-ofo/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/a2u22cX-ofo/">Rotors (Helicopters) -- Aerodynamics</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
