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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Aerodynamic damping and oscillatory stability in pitch and yaw of Gemini abort and reentry configurations at transonic and supersonic speeds
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of negative dihedral horizontal tail
Aerodynamic characteristics in pitch of variable sweep V/STOL configurations tested in supersonic wind tunnel
Analog computer program for parametric study of factors influencing deep stall pitch-up characteristics of T-tail transport aircraft
Low speed wind tunnel testing of high aspect ratio variable sweep wing supersonic transport model for determining methods of reducing pitch-up tendency
Pitch modulation maneuver for spacecraft reentry
Mathematical expressions derived for application of wind tunnel wall corrections to pitching moments caused by tail of aircraft model
Environmental testing and static firing of pitch control motor for Apollo spacecraft launch escape system
Flight simulator study of pitch maneuver speed margins for variable-sweep wing supersonic transport configuration
Linear segment pitch rate program for near optimum trajectory for rocket boosters
Drag coefficients used to evaluate normal force and pitching moment characteristics of revolving body at angle of attack
An analysis was made to determine the applicability of existing propeller theory and the theory of oscillating airfoils to the problem of determining the magnitude of the forces on propellers in pitch or yaw. Strip calculations using compressible airfoil characteristics were first made as though steady-state conditions existed successively at several blade positions of the propeller blades during one revolution. A theory of oscillating airfoils in pulsating incompressible potential flow was then considered from which it was possible to determine factors which would modify the steady-state forces.
The Design Guideline 03 (DG03) published by the National Renewable Energy Laboratory in 2009 is widely used in the wind industry. It allows engineers to get acquainted with design aspects and methodologies to determine pitch and yaw bearing static capacity and fatigue life. The combination of the detailed theoretical descriptions and practical examples makes it a highly application-oriented document. Since its publication, the knowledge about oscillating bearings, slewing bearings, and wind turbines has grown significantly. Some aspects of the DG03 need updates to reflect the current state of the art. This work covers proposed changes for an upcoming revision of DG03.
A Direct Adaptive Disturbance Rejection (DADR) control algorithm is evaluated using a numer-ical simulation of an Ocean Current Turbine (OCT) for its ability to minimize the cyclic loadings on the rotor blades caused by current shear. This control algorithm reduces these cyclic loadings by individually altering the pitch angles of the rotor blades as a function of rotor rotation angle. The OCT numerical model represents a system with a single 3 bladed 20 meter diameter rotor operated in the Gulf Stream off the coast of Ft. Lauderdale, Florida for mean and maximum measured current shear values of 0.004 and 0.03 (m/s)/m. The results indicate that the adaptive controller reduced the amplitude of the cyclic axial blade loads on a rigidly mounted and moored turbine by 91.18% and 92.3% in the mean current shear and by 94.12% and 81.88% in maximum current shear demonstrating the value of this controls approach.
This article discusses the development of an optimal variable-pitch controller for floating, axial-flow marine turbines. Recently, OpenFAST, an open-source wind turbine modeling tool, has been extended to model marine turbines. A controller is necessary to simulate marine turbines for different load cases using OpenFAST, which greatly impacts the performance of the energy system. Previous studies have designed controllers using a linearized model of the marine turbine, which can be timeconsuming and require the expertise of a control engineer. In this study, we use an automated approach that uses generic models of the marine turbine to identify the controller gains, which can expedite the process of designing a controller. Using an optimizer to identify the control system parameters can additionally improve the controller's performance. The optimal controller tuned using such an approach results in a 20% reduction in the towerbase damage equivalent loading and better tracking of the rated generator speed and power.
Carbon fibers (CF) with radial and random microstructures are produced. Here, these fibers are subjected to identical treatment before being mechanically tested and analyzed with Weibull analysis, with the results revealing a statistically significant difference in tensile strengths of 2.23 GPa for random CF and 1.69 GPa for radial CF. Raman mapping probed the crystalline structure perpendicular to the fiber axis and found a uniform structure, while wide‐angle X‐ray diffraction showed a significant difference of 7.5 Å in the crystallites’ basal lengths parallel to the fiber. Small‐angle X‐ray scattering is completed parallel to the fiber for the first time. A cross‐section Guinier plot of the 1D azimuthal integration is generated assuming symmetric scattering, and the parallel scatterers are found to have a similar length scale to the crystallite's length, validating the testing method. Finally, transmission electron microscopy is completed on the longitudinal cross‐section of each fiber. The radial carbon fiber is found to have a core–shell structure, as evidenced further by fast Fourier transform images. Through all studies, it is shown that the structure developed during mesophase pitch spinning altered the microstructure, thus impacting the mechanical properties, confirming a direct relationship between processing, structure, and properties.
Here, planar n-in-n silicon detectors with small pitches and slim edges are being investigated for the innermost layers of tracking devices for the foreseen upgrades of the LHC experiments. Sensor prototypes compatible with the CMS readout, fabricated by Sintef, were tested in the laboratory and with a 120 GeV/c proton beam at the Fermilab test beam facility before and after irradiation with up to 2 × 10 15 neq/cm 2 fluence. Preliminary results of the data analysis are presented.
Differential scanning calorimetry (DSC) was used to study the fast aging behavior of two petroleum pitch materials despite being only three to five years old.