364 research outputs found
Analytical and experimental investigation of circulation control by means of a turbulent Coanda jet
An analytical and experimental investigation of circulation control on a circular cylinder by means of tangential blowing (Coanda effect) is presented. The analytical method developed has also been used to estimate the blowing coefficients required for achieving potential flow on airfoils with flaps. The analysis is presented for conditions for which the flow in the boundary layer ahead of the jet exit is turbulent. The turbulent boundary layer and the jet layer on the upper surface, and the turbulent boundary layer on the lower surface are computed by a multi-strip integral method. The region of integration is between the correponding transition and separation points on each surface. Longitudinal curvature effects, which give rise to a radial pressure gradient across the jet layer and to an additional adverse tangential pressure gradient just upstream of the separation point, are included in the jet layer analysis in an approximate manner. The longitudinal curvature effect is found to have a pronounced influence on the separation of the jet layer
Nonlinear lift and pressure distribution of slender conical bodies with strakes at low speeds
Nonlinear lift and pressure distribution of slender conical bodies with strakes at low spee
Nonconical theory of flow past slender wing bodies with leading-edge separation
Nonconical theory of flow past slender wing bodies with leading edge separatio
Investigation of the stability, radiation, and structure of laminar coflow diffusion flames of CH4/NH3 mixtures
The stability, radiation, and structure of laminar axisymmetric CH4/NH3/air diffusion flames have been studied using photographic images, spectrally resolved measurements of flame radiation, and the spatial distribution of temperature and major species mole fractions obtained by spontaneous Raman scattering. The fit procedure for the Raman spectra of NH3 includes a hitherto unquantified overtone feature, whose inclusion in the fit significantly improves the NH3 fraction obtained. Nitrogen is used to replace NH3 to separate chemical effects of NH3 addition from those due to dilution. The results show that NH3 addition drastically reduces radiation from carbon-containing species, with progressively increasing strong chemiluminescence from excited NO2 and NH2, indicating a substantial change in flame chemistry. While the Rayleigh/Mie scattering from soot particles is still observed in the Raman spectra at 28% NH3 addition, 46% NH3 in the fuel is seen to suppresses soot formation effectively. The measured axial and radial profiles of temperature and major species indicate a substantial contribution from radial transport from the reaction zone, seriously complicating the relation between composition, mixture fraction, and the corresponding equilibrium temperature and mole fractions
(Non)Equilibrium of OH and Differential Transport in MILD Combustion:Measured and Computed OH Fractions in a Laminar Methane/Nitrogen Jet in Hot Coflow
Spatial distributions of temperature, major species, and OH mole fractions under moderate or intense low-oxygen-dilution (MILD) conditions in a laminar-jet-in-hot-coflow configuration were measured using spontaneous Raman and laser-induced-fluorescence methods. A preheated mixture of 18% CH4/82% N2 at 1100 K was used as fuel, while the products of a laminar, flat, premixed burner-stabilized flame with an equivalence ratio of 0.8 at 1550 K were used as the oxidizer. For comparison, experiments replacing the fuel by pure N2 were also performed. The measurements are compared with the results of numerical simulations performed using the GRI-Mech 3.0 chemical mechanism and a multicomponent mixture-averaged transport model. Analysis of the data shows that the maximum axial and radial temperature and OH mole fraction occur on the lean side of the stoichiometric mixture fraction. MILD combustion generates maximum OH mole fractions of ∼700 ppm in the radial profiles close to the burner exit and ∼300 ppm along the centerline, more than five times lower than those measured in equivalent methane/air diffusion flames. Overall, good qualitative and quantitative agreement is found between the results of detailed computations and experiments, with the maximum differences observed in the axial OH profiles, which are just outside the estimated experimental uncertainty. Analysis of the computational results shows that differential diffusion hinders the use of the mixture fraction to estimate the equilibrium temperature and species fractions, causing an overestimation of the stoichiometric temperature by ∼200 K. Calculating the equilibrium quantities based on the local (computed) species fractions shows an axial temperature profile that differs from that experimentally/computationally determined by less than 25 K. The analysis further shows that the measured OH mole fractions are roughly three times higher than the (locally determined) equilibrium value
The effect of H<sub>2</sub>S addition to methane on the ignition and oxidation at high pressures
Experimental and Modeling Investigation of the Effectof H2S Addition to Methane on the Ignition and Oxidation at High Pressures
The
autoignition and oxidation behavior of CH<sub>4</sub>/H<sub>2</sub>S mixtures has been studied experimentally in a rapid compression
machine (RCM) and a high-pressure flow reactor. The RCM measurements
show that the addition of 1% H<sub>2</sub>S to methane reduces the
autoignition delay time by a factor of 2 at pressures ranging from
30 to 80 bar and temperatures from 930 to 1050 K. The flow reactor
experiments performed at 50 bar show that, for stoichiometric conditions,
a large fraction of H<sub>2</sub>S is already consumed at 600 K, while
temperatures above 750 K are needed to oxidize 10% methane. A detailed
chemical kinetic model has been established, describing the oxidation
of CH<sub>4</sub> and H<sub>2</sub>S as well as the formation and
consumption of organosulfuric species. Computations with the model
show good agreement with the ignition measurements, provided that
reactions of H<sub>2</sub>S and SH with peroxides (HO<sub>2</sub> and
CH<sub>3</sub>OO) are constrained. A comparison of the flow reactor
data to modeling predictions shows satisfactory agreement under stoichiometric
conditions, while at very reducing conditions, the model underestimates
the consumption of both H<sub>2</sub>S and CH<sub>4</sub>. Similar
to the RCM experiments, the presence of H<sub>2</sub>S is predicted
to promote oxidation of methane. Analysis of the calculations indicates
a significant interaction between the oxidation chemistry of H<sub>2</sub>S and CH<sub>4</sub>, but this chemistry is not well understood
at present. More work is desirable on the reactions of H<sub>2</sub>S and SH with peroxides (HO<sub>2</sub> and CH<sub>3</sub>OO) and
the formation and consumption of organosulfuric compounds
The protein product of the c-cbl protooncogene is phosphorylated after B cell receptor stimulation and binds the SH3 domain of Bruton's tyrosine kinase.
Task Force III: Perspectives on the allocation of limited resources in cardiovascular medicine
- …