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Showing 1 to 20 of 276 for “"transonic"”.

  1. Transonic thermal blooming

    … unity. However, the nonlinearities in the transonic equations cutoff the trend to infinity, and the values of the flow perturbation quantities are finite. The nonlinear equations with heat addition are transformed into simple linear algebraic equations through the specification of the …

    nps Repository record for Transonic thermal blooming (opens in a new tab)

  2. Flow in Multistage Transonic Compressors

    Transonic compressors are regularly used as part of the compression system in industrial gas turbines because their high operating speeds make them capable of producing high stage pressure ratios and they have a high efficiency. The flow inside a these compressors is inherently unsteady due to …

    cambridge Repository record for Flow in Multistage Transonic Compressors (opens in a new tab)

  3. Transonic aerodynamics of dense gases

    Transonic flow of dense gases for two-dimensional, steady state, flow over a NACA 0012 airfoil was predicted analytically. The computer code used to model the dense gas behavior was a modified version of Jameson's FLOS2 airfoil code. The modifications to the code enabled modeling the dense gas …

    vt Repository record for Transonic aerodynamics of dense gases (opens in a new tab)

  4. Flowfield measurements in a transonic turbine

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.

    mit Repository record for Flowfield measurements in a transonic turbine (opens in a new tab)

  5. Studies of Multipoint Optimization of Transonic Stators

    A Multidisciplinary Design Optimization code was developed for NASA Stator 37. 3 different RANS solvers, Spalart-Allmaras, K-ε, and K-ω, were compared to design data to determine which was the fastest without significant error. K-ω was shown to be the most accurate, while only being 13.3% slower …

    ku Repository record for Studies of Multipoint Optimization of Transonic Stators (opens in a new tab)

  6. Aerodynamic inverse design of transonic turbomachinery cascades

    … used to obtain a shock-free design of an impulse transonic cascade and of the ONERA transonic compressor cascade. A parametric study has shown that the blade profile is rather sensitive to the prescribed loading distributions and that, in most cases, a smooth loading distribution results in a …

    concordia Repository record for Aerodynamic inverse design of transonic turbomachinery cascades (opens in a new tab)

  7. Development of a transonic turbine cascade facility

    … describes the design and initial testing of a transonic turbine cascade facility. It is specifically concerned with the best way to obtain flow periodicity and repeatability through the cascade by the use of tailboards at the cascade exit. The problem of how to achieve flow periodicity and …

    vt Repository record for Development of a transonic turbine cascade facility (opens in a new tab)

  8. An Extended Calibration and Validation of a Slotted-Wall Transonic Wall-Interference Correction Method for the National Transonic Facility

    … varying levels of ventilation at the National Transonic Facility (NTF) were modeled and calibrated with a general slotted wall (GSW) linear boundary condition to validate the computational model used to determine wall interference corrections. Free-air lift, drag, and pitching moment …

    vt Repository record for An Extended Calibration and Validation of a Slotted-Wall Transonic Wall-Interference Correction Method for the National Transonic Facility (opens in a new tab)

  9. Cascade wind tunnel for transonic compressor blading studies.

    The design and construction of a small, transonic, cascade wind tunnel are reported. The tunnel is of the intermittent blow-down type, and the initial test cascade models the flow at the rotor blade tips of a single stage transonic compressor at a relative Mach number of 1.U-. General programs were …

    nps Repository record for Cascade wind tunnel for transonic compressor blading studies. (opens in a new tab)

  10. Designing Shock Control Bumps for Transonic Commercial Aircraft

    … considered promising flow control devices for transonic commercial aircraft. By generating a λ-shock structure, 2D SCBs offer large drag savings, but perform poorly when that structure breaks down off-design. Milder-performing 3D devices produce weak vortices, that may offer some boundary layer …

    cambridge Repository record for Designing Shock Control Bumps for Transonic Commercial Aircraft (opens in a new tab)

  11. Newton solution of steady two-dimensional transonic flow

    Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.

    mit Repository record for Newton solution of steady two-dimensional transonic flow (opens in a new tab)

  12. Newton solution of steady two-dimensional transonic flow

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.

    mit Repository record for Newton solution of steady two-dimensional transonic flow (opens in a new tab)

  13. Unsteady radial transport in a transonic compressor stage

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

    mit Repository record for Unsteady radial transport in a transonic compressor stage (opens in a new tab)

  14. Transonic aeroelastic analysis of systems with structural nonlinearities

    … characteristics. Aerodynamic flows at transonic Mach numbers generate nonlinear aerodynamic forces on the wing affecting the aeroelastic response of the wing. Analysis techniques accounting for these structural and aerodynamic nonlinearities, and an understanding of their potential …

    vt Repository record for Transonic aeroelastic analysis of systems with structural nonlinearities (opens in a new tab)

  15. Efficient and robust design optimization of transonic airfoils

    … have been employed for the design of airfoils in transonic flow based on the transonic small-disturbance (TSD) and Euler equations. A sequential approximation optimization technique was implemented for solving the design problem of lift maximization with wave drag and area constraints. A simple …

    vt Repository record for Efficient and robust design optimization of transonic airfoils (opens in a new tab)

  16. Flow randomness and tip losses in transonic rotors

    The flowfields of two axial-flow fans and one core compressor are studied in this thesis. The research data, previously gathered by other researchers, was obtained by means of a high-response dual hot wire aspirating probe. The probe measures total pressure and total temperature (and thereby …

    vt Repository record for Flow randomness and tip losses in transonic rotors (opens in a new tab)

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