Generation of flow fields in particle fueled combustion systems Technical note no. 1
Dynamic properties of explosion in medium consisting of condensed phase fuel particles dispersed in gaseous oxidizer
GAS PHASE↗
SEARCH · Engineering Papers
Results for “flow field”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Analysis of the trajectory, loads and heating experienced by a body passing through a supersonic flow field
Analytical methods for determination of trajectories, loads, and heating experienced by spacecraft passing through rocket exhaust field
ROCKET EXHAUST↗
The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume analysis
Edelman, R.↗
Flow field computations for blunt bodies in planetary environments /equilibrium/ Final report
Radiative and convective heat transfer about two blunt bodies traveling at hypersonic speeds at zero angle of attack in assumed Mars atmosphere of nitrogen and carbon dioxide
Dohner, C. V.↗
ATM optical contamination study - Reaction control system rocket engine space plume flow fields Interim report
Apollo telescopic experiment contamination by space vehicle exhaust products
Chou, C. Y.↗
Determination of the flow field of an ideal axisymmetric impinging jet.
Axisymmetric jet impingement against solid plane from tube at finite distance, using nonlinear partial differential equation in finite difference form
Fisher, G. D.↗
Static aerodynamics, flow fields and aerodynamic heating of space shuttle orbiters
Wind tunnel tests of aerodynamic stability, boundary layer transition, and heat transfer in space shuttle orbiters
Axelson, J. A.↗
Viscous radiating flow field on an ablating blunt body
Viscous radiating flowfield coupled with ablation for computations on blunt body entering earth atmosphere at interplanetary return velocities
Graves, R. A., Jr.↗
Wind-tunnel measurement of static forces on internally carried bombs of two different bluff shapes in the flow field of a swept-wing fighter-bomber configuration at a Mach number of 1.6
Explore the source record for details and available documents.
Geier, D. J.↗
Injection, distribution, and evaporation of liquids in the flow fields of hypersonic vehicles
Explore the source record for details and available documents.
Beckwith, I. E.↗
Prediction of far flow field in trailing vortices.
A finite-difference machine code is brought to bear on the wake-vortex problem in the quasi-cylindrical boundary-layer approximation. A turbulent-energy model containing new features is developed. Parameters of the model are evaluated by comparison of calculated velocities and turbulent intensities with measurements in an axisymmetric wake. Comparisons are made with a previous calculation of the decay of an isolated vortex and with wind tunnel and flight measurements in trailing vortices. A self-similar solution develops at large axial distance that decays with the square root of distance. A slower decay occurs in the preceding transition region.
Baldwin, B. S.↗
Flow fields, pressure distributions, and heat transfer for delta wings at hypersonic speeds
Explore the source record for details and available documents.
Bertram, M. H.↗
Decay of far flow field in trailing vortices
A finite-difference machine code is brought to bear on the wake-vortex problem in the quasi-cylindrical boundary-layer approxmation. A turbulent-energy model containing new features is developed that accounts for the major effects disclosed by more advanced models in which the parameters are not yet established. Several puzzles are resolved that arose in previous theoretical investigations of wake vortices.
Baldwin, B. S.↗
Gudunov-method computation of the flow field associated with a sonic-boom focus.
Explore the source record for details and available documents.
Parker, L. W.↗
Analytical investigation of compressibility and three-dimensionality on the unsteady response of an airfoil in a fluctuating flow field.
Explore the source record for details and available documents.
Adamczyk, J. J.↗
Research on the sonic boom problem. Part 2: Flow field measurement in wind tunnel and calculation of second order F-function
An experimental investigation has been carried out in a wind tunnel to test some of the results of Landahl's second order theory. The slender models consisted of a parabolic spindle, tested at M = 3, and a wing body configuration, suggested by Ferri, and tested at M = 2.7. The theory indicates that shock position and strength at an arbitrary distance can be calculated by means of near field measurements. The results show that this method is an appropriate one for simple bodies and for bodies with complicated geometries as well.
Landahl, M.↗