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Showing 1 to 19 of 19 for “"Wind Tunnel Model"”.

  1. Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems

    … Institute and State University a flexible wing wind tunnel model was designed and constructed as a test article for the Luna Technologies Inc. fiber optic shape sensing system. In order to prove the capability of a fiber optic shape sensing system in a wind tunnel environment a flexible wing …

    vt Repository record for Analysis, Design and Testing of a Wind Tunnel Model to Validate Fiber-Optic Shape Sensing Systems (opens in a new tab)

  2. Evaluation of propulsor aerodynamic performance for powered aircraft wind tunnel experiments

    … mechanical ow power for a 1:11-scale, powered wind tunnel model of an advanced civil aircraft utilizing boundary layer ingestion (BLI); mechanical ow power is a surrogate for aircraft fuel burn. Back-to-back experiments of BLI and non-BLI aircraft configurations to assess the BLI benet directly …

    mit Repository record for Evaluation of propulsor aerodynamic performance for powered aircraft wind tunnel experiments (opens in a new tab)

  3. Qualitative Methods Used to Develop and Characterize the Circulation Control System on Cal Poly's AMELIA

    … control system onboard Cal Poly's Advanced Model for Extreme Lift and Improved Aeroacoustics was a critical component of a highly complex wind tunnel model produced in order to fulfill the requirements of a NASA Research Announcement awarded to David Marshall of the Aerospace Engineering …

    calpoly Repository record for Qualitative Methods Used to Develop and Characterize the Circulation Control System on Cal Poly's AMELIA (opens in a new tab)

  4. Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation

    … relative to a rigid airframe. An aircraft wind tunnel model with considerable wing-shape freedom can serve as a tool in learning to model, control, and fully exploit the potential of such vehicles. This work describes the design, development, and initial analysis of a wind tunnel model that …

    vt Repository record for Design, Development, and Analysis of a Morphing Aircraft Model for Wind Tunnel Experimentation (opens in a new tab)

  5. Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests

    … with a sensing head that was flush with the model wall and surrounded by a small gap. Thus, the shear force due to the flow along the wall deflects the head, inducing a measurable strain. Strain gages were used to detect the strain. The gages were statically calibrated using a direct force …

    vt Repository record for Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests (opens in a new tab)

  6. Investigation of a grid induced turbulent environment for wind tunnel testing

    In performing wind tunnel model tests of a two-dimensional nature, a grid constructed of 3.6 x 0.75 inch boards on 18 inch centers was used at the entrance of the tunnel. Important properties of the turbulent flow behind the uniform coarse grid were determined. The flow was found to be quite …

    vt Repository record for Investigation of a grid induced turbulent environment for wind tunnel testing (opens in a new tab)

  7. Dynamic control of aerodynamic forces on a moving platform using active flow control

    … motion in pitch and plunge is investigated in wind tunnel experiments using a two degree-of-freedom traverse which enables application of time-dependent external torque and forces by servo motors. The global aerodynamic forces and moments are regulated by controlling vorticity generation and …

    gatech Repository record for Dynamic control of aerodynamic forces on a moving platform using active flow control (opens in a new tab)

  8. Reentry Vehicle Aerodynamics and Control at Very High Angle of Attack

    … at the University of Illinois using a scale model of the X-38 to explore the cause of this problem. A six-component sting balance was used to measure the forces and moments on the 4.7% wind tunnel model at angles of attack from -7° to 95°. In addition, surface pressure taps and flow …

    uiuc Repository record for Reentry Vehicle Aerodynamics and Control at Very High Angle of Attack (opens in a new tab)

  9. An Experimental Investigation of Blown-Flap Airfoils

    … blowing enabled aircraft. A quasi 2-dimensional wind tunnel model is used to conduct surveys on both the performance and flow characteristics of propeller blown-flap airfoils. These surveys produced accurate estimates for the cₗ,cₓ,cₘ performance of these wings as a function of the test …

    mit Repository record for An Experimental Investigation of Blown-Flap Airfoils (opens in a new tab)

  10. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft

    … dynamics (CFD). From this initial analysis, a wind tunnel model is constructed and the systems are tested across the operating conditions required to characterize the performance of a VTOL aircraft, where 0 deg ≤ α ≤ 90 deg. One of these configurations is selected for evaluating the interaction …

    syracuse-diss Repository record for Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft (opens in a new tab)

  11. An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design

    … and moment data were obtained in two separate wind tunnel test entries in the VPI Stability Tunnel. The first of these entries were concerned with longitudinal characteristics while the second dealt primarily with lateral/directional characteristics. Flow visualization was also done in both …

    vt Repository record for An experimental and computational aerodynamic investigation of a low-canard high-wing aircraft design (opens in a new tab)

  12. Wind loads for petrochemical structures

    … available to practicing engineers for estimating wind loads for petrochemical structures have little theoretical or experimental basis. This dissertation research is an effort to expand the understanding of wind effects on petrochemical and other, similar structures. Petrochemical structures …

    lsu-thes Repository record for Wind loads for petrochemical structures (opens in a new tab)

  13. Stability enhancement of a transonic wing using a passive nonlinear energy sink

    … of transonic aeroelastic instabilities of a wind-tunnel model wing. Medium- and high-fidelity computational aeroelastic models were used to study the transonic aeroelastic instabilities of the wing and to design a nonlinear energy sink (NES) to enhance stability. Several flutter-suppression …

    uiuc Repository record for Stability enhancement of a transonic wing using a passive nonlinear energy sink (opens in a new tab)

  14. An Application of Anti-Optimization in the Process of Validating Aerodynamic Codes

    … wing was designed for the experiment. A wind tunnel model of this wing was built and tested in the NASA Langley Transonic Dynamics Tunnel. Selection of the test conditions (i.e., Mach and Reynolds numbers) were made by applying the techniques of response surface methodology and …

    vt Repository record for An Application of Anti-Optimization in the Process of Validating Aerodynamic Codes (opens in a new tab)

  15. A computer program for an equation of wind velocity profiles from zero to thirty feet

    … of the structure and nature of natural wind and to the development of theories which can be applied to the design of buildings and other structures. Extensive studies of the velocity profile of wind have been made from the ground to the stratosphere, but investigators have concentrated …

    vt Repository record for A computer program for an equation of wind velocity profiles from zero to thirty feet (opens in a new tab)

  16. Air jet vortex generators for wind turbines

    … is less than the air jets 'on' stall angle. A wind tunnel model was built and tested and then modified to incorporate air jets. The air jets increased CL max by 55% and reduced the drag throughout the incidence range, a, for the chosen blowing pressure of 1 p. s. i. (6900Pa). By varying the air …

    city-london Repository record for Air jet vortex generators for wind turbines (opens in a new tab)

  17. Experiments on the stability of the flat-plate boundary layer with suction

    … The experiments were conducted on a flat-plate wind-tunnel model in the V.P.I. & S.U. Stability Tunnel. The capabilities of the wind tunnel in terms of mean flow uniformity and low turbulence level were established and the basic flat-plate experiment was verified by comparison with the well …

    vt Repository record for Experiments on the stability of the flat-plate boundary layer with suction (opens in a new tab)

  18. Eddy-resolving simulations of the flow around a vertical tail plane

    … investigation carried out in this thesis uses a wind tunnel model tested at Airbus. The study starts with steady RANS approaches for different turbulence models. RANS simulations produce acceptable results for the flow at low incidence levels. On the contrary, at high incidence, when flow …

    cambridge Repository record for Eddy-resolving simulations of the flow around a vertical tail plane (opens in a new tab)

  19. Vertical axis wind turbine acoustics

    … decentralised power generation. Small-scale wind power has seen significant growth in the last ten years, partly due to the political support for renewable energy and the introduction of Feed In Tariffs, which pay home owners for generating their own electricity. Due to their ability to …

    cambridge Repository record for Vertical axis wind turbine acoustics (opens in a new tab)