5,298 research outputs found

    Study of effects of injector geometry on fuel-air mixing and combustion

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    An implicit finite-difference method has been developed for computing the flow in the near field of a fuel injector as part of a broader study of the effects of fuel injector geometry on fuel-air mixing and combustion. Detailed numerical results have been obtained for cases of laminar and turbulent flow without base injection, corresponding to the supersonic base flow problem. These numerical results indicated that the method is stable and convergent, and that significant savings in computer time can be achieved, compared with explicit methods

    Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance

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    Described here is the development of a flexible simulation model for scramjet hypersonic propulsion systems. The primary goal is determination of sensitivity of the thrust vector and other system parameters to angle of attack changes of the vehicle. Such information is crucial in design and analysis of control system performance for hypersonic vehicles. The code is also intended to be a key element in carrying out dynamic interaction studies involving the influence of vehicle vibrations on propulsion system/control system coupling and flight stability. Simple models are employed to represent the various processes comprising the propulsion system. A method of characteristics (MOC) approach is used to solve the forebody and external nozzle flow fields. This results in a very fast computational algorithm capable of carrying out the vast number of simulation computations needed in guidance, stability, and control studies. The three-dimensional fore- and aft body (nozzle) geometry is characterized by the centerline profiles as represented by a series of coordinate points and body cross-section curvature. The engine module geometry is represented by an adjustable vertical grid to accommodate variations of the field parameters throughout the inlet and combustor. The scramjet inlet is modeled as a two-dimensional supersonic flow containing adjustable sidewall wedges and multiple fuel injection struts. The inlet geometry including the sidewall wedge angles, the number of injection struts, their sweepback relative to the vehicle reference line, and strut cross-section are user selectable. Combustion is currently represented by a Rayleigh line calculation including corrections for variable gas properties; improved models are being developed for this important element of the propulsion flow field. The program generates (1) variation of thrust magnitude and direction with angle of attack, (2) pitching moment and line of action of the thrust vector, (3) pressure and temperature distributions throughout the system, and (4) performance parameters such as thrust coefficient, specific impulse, mass flow rates, and equivalence ratio. Preliminary results are in good agreement with available performance data for systems resembling the NASP vehicle configuration

    Using the local gyrokinetic code, GS2, to investigate global ITG modes in tokamaks. (I) s-α{\alpha} model with profile and flow shear effects

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    This paper combines results from a local gyrokinetic code with analytical theory to reconstruct the global eigenmode structure of the linearly unstable ion-temperature-gradient (ITG) mode with adiabatic electrons. The simulations presented here employ the s-α{\alpha} tokamak equilibrium model. Local gyrokinetic calculations, using GS2 have been performed over a range of radial surfaces, x, and for ballooning phase angle, p, in the range -π≤p≤π{\pi} {\leq} p {\leq\pi}, to map out the complex local mode frequency, Ω0(x,p)=ω0(x,p)+iγ0(x,p){\Omega_0(x, p) = \omega_0(x, p) + i\gamma_0(x, p)}. Assuming a quadratic radial profile for the drive, namely ηi=Ln/LT{\eta_i = L_n/L_T}, (holding constant all other equilibrium profiles such as safety factor, magnetic shear etc.), Ω0(x,p){\Omega_0(x, p)} has a stationary point. The reconstructed global mode then sits on the outboard mid plane of the tokamak plasma, and is known as a conventional or isolated mode, with global growth rate, γ{\gamma} ~ Max[γ0(x,p){\gamma_0(x, p)}], where γ0(x,p){\gamma_0(x, p)} is the local growth rate. Taking the radial variation in other equilibrium profiles (e.g safety factor q(x)) into account, removes the stationary point in Ω0(x,p){\Omega_0(x, p)} and results in a mode that peaks slightly away from the outboard mid-plane with a reduced global growth rate. Finally, the influence of flow shear has also been investigated through a Doppler shift, ω0→ω0+nΩ′x{\omega_0 \rightarrow \omega_0 + n\Omega^{\prime}x}, where n is the toroidal mode number and Ω′{\Omega^{\prime}} incorporates the effect of flow shear. The equilibrium profile variation introduces an asymmetry to the growth rate spectrum with respect to the sign of Ω′{\Omega^{\prime}}, consistent with recent global gyrokinetic calculations.Comment: 10 pages, 8 figures and 1 tabl

    Structure of Micro-instabilities in Tokamak Plasmas: Stiff Transport or Plasma Eruptions?

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    Solutions to a model 2D eigenmode equation describing micro-instabilities in tokamak plasmas are presented that demonstrate a sensitivity of the mode structure and stability to plasma profiles. In narrow regions of parameter space, with special plasma profiles, a maximally unstable mode is found that balloons on the outboard side of the tokamak. This corresponds to the conventional picture of a ballooning mode. However, for most profiles this mode cannot exist and instead a more stable mode is found that balloons closer to the top or bottom of the plasma. Good quantitative agreement with a 1D ballooning analysis is found provided the constraints associated with higher order profile effects, often neglected, are taken into account. A sudden transition from this general mode to the more unstable ballooning mode can occur for a critical flow shear, providing a candidate model for why some experiments observe small plasma eruptions (Edge Localised Modes, or ELMs) in place of large Type I ELMs.Comment: 11 pages, 3 figure

    A study of ASRS reports involving general aviation and weather encounters

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    Consideration is given to the nature and characteristics of problems involving dissemination of weather information, use of this information by pilots, its adequacy for the purpose intended, the ability of the air traffic control system to cope with weather related incidents, and the various aspects of pilot behavior, aircraft equipment, and NAVAIDS affecting flights in which weather figures. It is concluded from the study that skill and training deficiencies of general aviation pilots are not major factors in weather related occurrences, nor is lack of aircraft equipment. Major problem causes are identified with timely and easily interpreted weather information, judgement and attitude factors of pilots, and the functioning of the air traffic control system

    A Community Project to Supplement Social Care Services

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    Solva in West Wales, UK, is a small community with about 700 people on the electoral roll. In 2013, Solva Community Council faced the fact that things were not going well for the elderly in our village. Many had to leave home and go "into care." They didn't want to go and we didn't want to lose them. A community councillor at that time, author Mollie Roach, did some research and decided that the village could look after its own. A small working party including first author Frances Barker was set up to plan the way forward. The original idea was not a volunteer service. We wanted to set up a local domiciliary care service, where the carers would live locally and not have to spend their precious time travelling between wide-spread destinations. We soon found that there were several administrative and monetary barriers in the way of setting up such a scheme, especially for a small community. Registration needed money and qualified people. and the "rules" were such as to prevent rather than encourage individual response to individual circumstances. However, we could see that there was a need for a local volunteer service. It is disturbing when you discover you cannot go up a ladder and change a light bulb. It is devastating when you are told you cannot drive anymore because of an eye problem. It is worrying when you cannot take the dog for a good walk or collect your prescription because of arthritis. All these problems are under the radar of statutory services. This is a gap that can be alleviated by a local community-based volunteer scheme. Solva Care evolved with a paid co-ordinator to mediate between volunteers and those needing help. We are now getting closer to the original idea, doing our best to integrate domiciliary and social care, working with agencies, private carers, families, and individuals, as well as continuing to run the volunteer service

    Kinetic instabilities that limit {\beta} in the edge of a tokamak plasma: a picture of an H-mode pedestal

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    Plasma equilibria reconstructed from the Mega-Amp Spherical Tokamak (MAST) have sufficient resolution to capture plasma evolution during the short period between edge-localized modes (ELMs). Immediately after the ELM steep gradients in pressure, P, and density, ne, form pedestals close to the separatrix, and they then expand into the core. Local gyrokinetic analysis over the ELM cycle reveals the dominant microinstabilities at perpendicular wavelengths of the order of the ion Larmor radius. These are kinetic ballooning modes (KBMs) in the pedestal and microtearing modes (MTMs) in the core close to the pedestal top. The evolving growth rate spectra, supported by gyrokinetic analysis using artificial local equilibrium scans, suggest a new physical picture for the formation and arrest of this pedestal.Comment: Final version as it appeared in PRL (March 2012). Minor improvements include: shortened abstract, and better colour table for figures. 4 pages, 6 figure
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