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Showing 1 to 5 of 5 for “"Wind Tunnel Design"”.

  1. An experimental investigation of unsteady separation shock wave motion in a plume-induced, separated flowfield

    … PIBLS flowfields were created in a blowdown-type wind tunnel designed specifically to produce PIBLS in a planar, two-stream, supersonic flow. In this unique wind tunnel, separation of the freestream boundary layer upstream of the base plane was accomplished by utilizing an angle-induced separation …

    uiuc Repository record for An experimental investigation of unsteady separation shock wave motion in a plume-induced, separated flowfield (opens in a new tab)

  2. Design and flow characterization of an indraft supersonic wind tunnel for scramjet testing

    … the Colorado State University supersonic wind tunnel design, manufacture, assembly, and validation. The overarching goal of this research is to develop a ground testing platform for studying airbreathing hypersonic propulsion systems. Problems of interest include design of isolators, fuel …

    colostate Repository record for Design and flow characterization of an indraft supersonic wind tunnel for scramjet testing (opens in a new tab)

  3. Rigorous Design of a Compact, Low-Speed, Open-Loop Wind Tunnel

    Currently available literature regarding the design of fluid flow systems tend to focus on the specific system without providing a general guideline for how to address the design problem. This thesis focuses on developing such a general approach which is applied to the design of a wind tunnel meant …

    windsor Repository record for Rigorous Design of a Compact, Low-Speed, Open-Loop Wind Tunnel (opens in a new tab)

  4. The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments

    A supersonic wind tunnel, with a 20" x 20'" test section cross sectional area, was designed and constructed at the Techsburg Wind Tunnel Facility in order to determine the lift and drag on irregularly shaped fragments in supersonic flow. Prior to beginning the wind tunnel design process, a blowdown …

    vt Repository record for The Design and Construction of a 20" x 20" Mach 2.0 Blowdown Wind Tunnel to Characterize the Lift and Drag of Irregularly Shaped Fragments (opens in a new tab)

  5. Wind tunnel test section design active flow control implementation

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-10-19 without embargo terms

    uiuc Repository record for Wind tunnel test section design active flow control implementation (opens in a new tab)