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  • 1
    Publication Date: 2006-04-20
    Description: Sonic jet injection into subsonic free stream
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANALYSIS OF A JET IN A SUBSONIC CROSSWIND 1969; P 63-84
    Format: text
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  • 2
    Publication Date: 2019-06-27
    Description: A flow model has been developed to study the flow development after reattachment with supersonic external streams. Special attention is given to the pressure difference across the viscous layer, and it is suggested that such a flow redevelopment can be treated as a relaxation of this pressure difference. Upon correlating the pressure difference with a slope parameter of the velocity profile, the system of equations governing the flow would produce a saddle point singularity corresponding to the fully rehabilitated asymptotic flow condition. A method of calculation for this flowfield, in conjunction with the matching of the upstream flow, has been derived and is discussed. Samples of calculations are also presented. Reasonably good agreement with experimental data has also been observed.
    Keywords: AERODYNAMICS
    Type: AIAA Journal; 13; Dec. 197
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: Wind tunnel test results are presented to show aerodynamic characteristics over the Mach number range of 0.64 to 2.50 of the DCAT missile. Data are presented showing the interference created by the rear mounted reaction control system. Two candidate fins were installed on the model during tests: a flat folding fin and a curved wrap around fin.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-140750 , AD-784121 , RD-73-27
    Format: application/pdf
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  • 4
    Publication Date: 2019-06-27
    Description: A flow model has been devised to deal with the viscid-inviscid interaction of a class of two-dimensional incompressible separated flow problems. It is suggested that the corresponding inviscid flow of these problems is described by the free streamline theory with few unspecified parameters and their values are, in turn, determined by the viscous flow considerations. The problem of a flow past a backward facing step is selected for study in detail. The viscous flow components of turbulent jet mixing, recompression, and reattachment are delineated and studied individually. When they are later combined, it is found that the point of reattachment behaves as a saddle-point-type singularity in the system of differential equations describing the viscous flow process. This feature is employed to the determination of the aforementioned free parameters and thus the establishment of the overall corresponding inviscid flow field. The resulting base pressure coefficient for the specific case agrees reasonably well with the available experimental data.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 76-WA/APM-7
    Format: text
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