12 research outputs found

    A Sweeping Jet Application on a High Reynolds Number Semispan Supercritical Wing Configuration

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    The FAST-MAC circulation control model was modified to test an array of unsteady sweeping-jet actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Two types of sweeping jet actuators were fabricated using rapid prototype techniques, and directed over a 15% chord simple-hinged flap. The model was configured for low-speed high-lift testing with flap deflections of 30 and 60, and a transonic cruise configuration with a 0 flap deflection. For the 30 flap high-lift configuration, the sweeping jets achieved comparable lift performance in the separation control regime, while reducing the mass flow by 54% as compared to steady blowing. However, the sweeping jets were not effective for the 60 flap. For the transonic cruise configuration, the sweeping jets reduced the drag by 3.3% at an off design condition. The drag reduction for the design lift coefficient for the sweeping jets provided only half the drag reduction shown for the steady blowing case (6.5%), but accomplished this with a 74% reduction in mass flow

    Development of the Circulation Control Flow Scheme Used in the NTF Semi-Span FAST-MAC Model

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    The application of a circulation control system for high Reynolds numbers was experimentally validated with the Fundamental Aerodynamic Subsonic Transonic Modular Active Control semi-span model in the NASA Langley National Transonic Facility. This model utilized four independent flow paths to modify the lift and thrust performance of a representative advanced transport type of wing. The design of the internal flow paths highlights the challenges associated with high Reynolds number testing in a cryogenic pressurized wind tunnel. Weight flow boundaries for the air delivery system were identified at mildly cryogenic conditions ranging from 0.1 to 10 lbm/sec. Results from the test verified system performance and identified solutions associated with the weight-flow metering system that are linked to internal perforated plates used to achieve flow uniformity at the jet exit

    Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility

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    A second wind tunnel test of the FAST-MAC circulation control model was recently completed in the National Transonic Facility at the NASA Langley Research Center. The model was equipped with four onboard flow control valves allowing independent control of the circulation control plenums, which were directed over a 15% chord simple-hinged flap. The model was configured for low-speed high-lift testing with flap deflections of 30 and 60 degrees, along with the transonic cruise configuration with zero degree flap deflection. Testing was again conducted over a wide range of Mach numbers up to 0.88, and Reynolds numbers up to 30 million based on the mean chord. The first wind tunnel test had poor transonic force and moment data repeatability at mild cryogenic conditions due to inadequate thermal conditioning of the balance. The second test demonstrated that an improvement to the balance heating system significantly improved the transonic data repeatability, but also indicated further improvements are still needed. The low-speed highlift performance of the model was improved by testing various blowing slot heights, and the circulation control was again demonstrated to be effective in re-attaching the flow over the wing at off-design transonic conditions. A new tailored spanwise blowing technique was also demonstrated to be effective at transonic conditions with the benefit of reduced mass flow requirements

    Advantages of a Modular Mars Surface Habitat Approach

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    Early crewed Mars mission concepts developed by the National Aeronautics and Space Administration (NASA) assumed a single, large habitat would house six crew members for a 500-day Mars surface stay. At the end of the first mission, all surface equipment, including the habitat, -would be abandoned and the process would be repeated at a different Martian landing site. This work was documented in a series of NASA publications culminating with the Mars Design Reference Mission 5.0 (NASA-SP-2009-566). The Evolvable Mars Campaign (EMC) explored whether re-using surface equipment at a single landing site could be more affordable than the Apollo-style explore-abandon-repeat mission cadence. Initial EMC assumptions preserved the single, monolithic habitat, the only difference being a new requirement to reuse the surface habitat for multiple expedition crews. A trade study comparing a single large habitat versus smaller, modular habitats leaned towards the monolithic approach as more mass-efficient. More recent work has focused on the operational aspects of building up Mars surface infrastructure over multiple missions, and has identified compelling advantages of the modular approach that should be considered before making a final decision. This paper explores Mars surface mission operational concepts and integrated system analysis, and presents an argument for the modular habitat approach

    Spirituality expressed in creative learning: young children's imagining play as space for mediating their spirituality

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    Historically underpinning principles of the English curriculum framework for children from birth to five years explicitly acknowledged a spiritual dimension to children's uniqueness and well-being. Yet spirituality receives scant reference in the discourse of creative learning and teaching. This paper considers the relationship of spirituality to creativity and argues for a greater attentiveness to children's spirituality in early childhood education that acknowledges its presence in expression of children's thinking, creating and imagining. Located within an interpretive paradigm, this ethnographic study of children aged two and three years in a day nursery in England, explores how they express spirituality. A hermeneutic approach underpins the analysis and interpretation of the data. Findings reveal how in imaginative play, most often recognised in the early years curriculum as part of creative development, young children show a capacity for expressing meaning-making and negotiating identity, key dimensions of the spiritual in childhood

    Pastoral care for shame-based perfectionism

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    While perfectionism has been associated with guilt dynamics, the form of perfectionism that is most frequently discussed by psychologists is connected to self-condemnation for perceived failures to reach the high standard set for personal achievement. There is therefore a strong link between perfectionism and inferiority shame. Psychotherapists have given quite a bit of attention to shame-based perfectionism; it has been largely neglected by pastoral psychologists. Three approaches to the pastoral care of shame-based perfectionism are developed. The first approach is based in cognitive therapy. It is argued that perfectionism is grounded in a faulty core belief about the self—namely, “I am what I achieve.” The second method makes use of strategies developed by John Bradshaw for accepting and affirming all one’s sub-selves. Bradshaw’s approach is critiqued, however, for the way in which shame-based and guilt-based perfectionism are confused. The third method is a modification and adaptation of Heinz Kohut’s strategy of “mirroring” (empathy, admiration, and approval) that he developed for use in work with clients with narcissistic personality disorder
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