Rotors (Helicopters)
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The concept Rotors (Helicopters) represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Rotors (Helicopters)
Resource Information
The concept Rotors (Helicopters) represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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- Rotors (Helicopters)
46 Items that share the Concept Rotors (Helicopters)
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- [The application of experimental data to blade wake interaction noise prediction
- A study of the noise mechanisms of transonic blade-vortex interactions
- A three-dimensional viscous flow analysis for the helicopter tip vortex generation problem
- Aeroelastic loads and stability investigation of a full-scale hingeless rotor
- An experimental investigation of helicopter rotor hub fairing drag characteristics
- An experimental study of the sensitivity of helicopter rotor blade tracking to root pitch adjustment in hover
- Analysis of open loop higher harmonic control at high airspeeds on a modern four-bladed articulated rotor
- Analysis of small-scale rotor hover performance data
- Application of higher harmonic blade feathering on the OH-6A helicopter for vibration reduction
- Black Hawk helicopter vibration analysis due to main rotor damage : directional constituents of the resultant vibrations
- Certification of normal category rotorcraft
- Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight
- Control of helicopter rotorblade aerodynamics
- Correlation of AH-1G airframe flight vibration data with a coupled rotor-fuselage analysis
- Correlation of Puma airloads : lifting-line and wake calculation
- Correlation of airloads on a two-bladed helicopter rotor
- Coupled rotor-body equations of motion hover flight : interim report
- Effect of planform taper on hover performance of an advanced AH-64 model rotor
- Experimental study of performance degradation of a rotating system in the NASA Lewis RC icing tunnel : final technical report
- Foil bearing starting considerations and requirements for rotorcraft engine applications
- Full-scale transmission testing to evaluate advanced lubricants
- Icing research tunnel test of a model helicopter rotor
- Image-based ranging and guidance for rotorcraft
- Integration of dynamic, aerodynamic, and structural optimization of helicopter rotor blades : final report, NASA research grant no. NAG 1-1710 for period covering 15 October 1986 to 30 November 1991
- Integration of dynamic, aerodynamic, and structural optimization of helicopter rotor blades : second semi-annual status report NASA research grant no. NAG 1-710 for period covering 14 April 1987 to 13 October 1987
- Model helicopter rotor high-speed impulsive noise : measured acoustics and blade pressures
- Noise produced by turbulent flow into a rotor : theory manual for atmospheric turbulence prediction and mean flow and turbulence contraction prediction
- Ongoing development of a computer jobstream to predict helicopter main rotor performance in icing conditions
- Optimizing tuning masses for helicopter rotor blade vibration reduction including computed airloads and comparison with test data
- Performance and loads data from a hover test of a 0.658-scale V-22 rotor and wing
- Performance and loads data from a hover test of a full-scale advanced technology XV-15 rotor
- Performance optimization of helicopter rotor blades
- Periodic control of the individual-blade-control helicopter rotor
- Perpendicular blade vortex interaction and its implications for helicopter noise prediction : final report to NASA Langley on research performed under grant NAG-1-1119, "wave-number frequency spectra in a trailing vortex for BSI noise prediction" for the period ending 15th August, 1993
- Quiet mode for nonlinear rotor models
- Rotor and control system loads analysis of the XV-15 with the advanced technology blades
- Rotor design optimization using a free wake analysis
- Rotor induced-inflow-ratio measurements and CAMRAD calculations
- Technology needs for high-speed rotorcraft (I)
- The selection of convertible engines with current gas generator technology for high speed rotorcraft
- Tiltrotor research aircraft composite blade repairs : lessons learned
- Transonic blade-vortex interactions noise : a parametric study
- Transonic flow analysis for rotors : part 2, Three-dimensional, unsteady, full-potential calculation
- Transonic flow analysis for rotors, Part 3, Three-dimensional, quasi-steady, Euler calculation
- Unanticipated right yaw in helicopters
- Wake coupling to full potential rotor analysis code
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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.umsl.edu/resource/n6HKo-nBmwI/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/n6HKo-nBmwI/">Rotors (Helicopters)</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
