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  • 1995-1999  (1)
  • 1985-1989  (2)
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Years
Year
  • 1
    Electronic Resource
    Electronic Resource
    The application of inverse boundary layer methods to the three-dimensional viscous design problem (1986)
    New York, NY [u.a.] : Wiley-Blackwell
    Communications in Applied Numerical Methods 2 (1986), S. 57-61 
    Details
    ISSN: 0748-8025
    Keywords: Engineering ; Engineering General
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Mathematics , Technology
    Notes: The problem of designing three-dimensional configurations with specified skin friction is addressed. For wall flows that are boundary layers, the following procedure is described. The input skin friction is used as a target for an inverse boundary layer calculation. The resulting pressure distribution is used as input to an inviscid configuration design procedure. This procedure computes the body geometry. The procedure is demonstrated by modifying the lift of a wing section, in compressible flow.
    Additional Material: 4 Ill.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/cnm.1630020109
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    Paper (German National Licenses)
    Fulltext
  • 2
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    Numerical solution of unsteady rotational flow past fixed and rotary wing configurations (1989)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The application of unsteady 3-D Euler and Navier-Stokes equations to transonic flow past rotor blades, and wing-alone configurations is described. A promising approach for the numerical solution of these equations is examined. Additional work is needed for improving the efficiency of the present procedure. It is hoped that the techniques presented will find use in fixed and rotary wing aircraft analysis.
    Keywords: AERODYNAMICS
    Type: NASA, Langley Research Center, Transonic Unsteady Aerodynamics and Aeroelasticity 1987, Part 2; p 351-374
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    The Design of Future Airbreathing Engine Systems within an Intelligent Synthesis Environment (1999)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper describes a new Initiative proposed by the National Aeronautics and Space Administration (NASA). The purpose of this initiative is to develop a future design environment for engineering and science mission synthesis for use by NASA scientists and engineers. This new initiative is called the Intelligent Synthesis Environment (ISE). The paper describes the mission of NASA, future aerospace system characteristics, the current engineering design process, the ISE concept, and concludes with a description of possible ISE applications for the decision of air-breathing propulsion systems.
    Keywords: Aircraft Propulsion and Power
    Type: NASA/TM-1999-209192 , NAS 1.15:209192 , E-11706 , 14th International on Air Breathing Engines; Sep 05, 1999 - Sep 10, 1999; Florence; Italy
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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