NASA Technical Reports Server (NTRS) 19740010803: Flowfield Analysis For Successive Oblique Shock Wave Interactions With A Turbulent Boundary Layer - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19740010803: Flowfield Analysis For Successive Oblique Shock Wave Interactions With A Turbulent Boundary Layer" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19740010803: Flowfield Analysis For Successive Oblique Shock Wave Interactions With A Turbulent Boundary Layer” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19740010803: Flowfield Analysis For Successive Oblique Shock Wave Interactions With A Turbulent Boundary Layer
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19740010803
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"NASA Technical Reports Server (NTRS) 19740010803: Flowfield Analysis For Successive Oblique Shock Wave Interactions With A Turbulent Boundary Layer" Description:
The Internet Archive:
A computation procedure is described for predicting flow fields which develop when successive interactions between oblique shock waves and a turbulent boundary layer occur. Computations were carried out for axisymmetric internal flows at free stream Mach numbers = 3.82 and 2.82. The effect of boundary layer bleed was considered for the free stream Mach number = 2.82 flow. A control volume analysis is used to predict changes in the flow field across the interactions. Two bleed flow models were considered. A turbulent boundary layer program was used to compute changes in the boundary layer between the interactions. The results given are for flows with two shock wave interactions and for bleed at the second interaction site. In principle the method described may be extended to account for additional interactions. The predicted results are compared with measured results and are shown to be in good agreement when the bleed flow rate is low (on the order of 3 percent of the boundary layer mass flow), or when there is no bleed. As the bleed flow rate is increased, differences between the predicted and measured results become larger. Shortcomings of the bleed flow models at higher bleed flow rates are discussed.
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