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  • FLUID MECHANICS AND HEAT TRANSFER  (67)
  • INSTRUMENTATION AND PHOTOGRAPHY  (60)
  • 1980-1984  (127)
  • 1940-1944
  • 1983  (127)
Collection
Keywords
Years
  • 1980-1984  (127)
  • 1940-1944
Year
  • 1
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    Mean flowfields in axisymmetric combustor geometries with swirl (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: (Previously cited in issue 06, p. 860, Accession no. A82-17824)
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Short wavelength infrared hybrid focal plane arrays (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: The employment of area focal plane arrays (FPA) has made it possible to obtain second generation infrared imaging systems with high resolution and sensitivity. The Short Wavelength Infrared (SWIR) region (1-2.5 microns) is of importance for imaging objects at high temperature and under conditions of reflected sunlight. The present investigation is concerned with electrooptical characterization results for 32 x 32 SWIR detector arrays and FPAs which are suitable for use in a prototype imaging spectrometer. The employed detector material is Hg(1-x)Cd(x)Te grown by liquid phase epitaxy on a CdTe transparent substrate. Attention is given to details of processing, the design of the detector array, the multiplexer, the fabrication of the hybrid FPA, and aspects of performance.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: Technical issues in infrared detectors and arrays; April 5, 6, 1983; Arlington, VA
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Moire deflectometry with deferred analysis (1983)
    In:  Other Sources
    Details
    Publication Date: 2011-08-18
    Description: A simplified version of moire deflectometry for flow visualization is presented. The modification comprises replacement of the second grating, the ground glass screen, and the camera with a plate film holder to obtain a shadow picture. Postanalysis proceeds by placing a grid transparency of the same periodicity of the remaining glass grating on the negative for projection viewing. The rotational angle between the grating and the plate alters the moire fringe periodicity. Use of the method in studying flows is predicted to reveal weak density gradient areas and shocks.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: Applied Optics; 22; Mar. 1
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Ride quality meter (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A ride quality meter is disclosed that automatically transforms vibration and noise measurements into a single number index of passenger discomfort. The noise measurements are converted into a noise discomfort value. The vibrations are converted into single axis discomfort values which are then converted into a combined axis discomfort value. The combined axis discomfort value is corrected for time duration and then summed with the noise discomfort value to obtain a total discomfort value.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Spectral methods for the Euler equations (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Spectral methods for compressible flows are introduced in relation to finite difference and finite element techniques within the framework of the method of weighted residuals. Current spectral collocation methods are put in historical context. The basic concepts of both Fourier and Chebyshev spectral collocation methods are provided. Filtering strategies for both shock-fitting and shock-capturing approaches are also presented. Fourier shock capturing techniques are evaluated using a one-dimensional, periodic astrophysical 'nozzle' problem. Examples of shock-fitting approaches include a shock/acoustic wave interaction, shock/vortex interaction, and the classical blunt body problem. While the shock capturing spectral method does not yet show a clear advantage over second-order finite differences, equivalent accuracy can be obtained using shock fitting with far fewer grid points.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: AIAA PAPER 83-1942
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Laser diagnostic methods - A summary (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: This is a summary and discussion of the state of the art in the use of laser diagnostics in fluid and plasma dynamics. This will encompass: interferometry, scattering, spectroscopy, and velocimetry. Examples of such applications will be provided in the area of fluid dynamics of particle generation and breakup, analysis of three-dimensional density fields, and applications in combustion.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: AIAA PAPER 83-1683
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    NASA TECHNICAL REPORTS
  • 7
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    Apparatus for continuous, fast, and precise measurements of position and velocity of a small spherical particle (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The position and velocity of optically levitated glass spheres (radii 10-20 microns) movng in a gas are measured accurately, rapidly, and continuously using a high-speed rotating polygon mirror. The experimental technique developed here has repeatable position accuracies better than 20 microns. Each measurement takes less than 1 microsec and can be repeated every 100 microsec. The position of the levitated glass spheres can be manipulated accurately by modulating the laser power with an acoustic optic modulator. The technique provides a fast and accurate method to study general particle dynamics in a fluid.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: Review of Scientific Instruments (ISSN 0034-6748); 54; 1643-164
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    NASA TECHNICAL REPORTS
  • 8
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    Remote sensing of sediment and chlorophyll with the test-bed aircraft multispectral scanner (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An instrument known as the test-bed aircraft multispectral scanner (TBAMS) was used in a research flight over the entrance to the Chesapeake Bay. Upwelled radiances from the TBAMS data were correlated with the water parameters, particularly sediment and chlorophyll a. Several algorithms were demonstrated for monitoring sediment and chlorophyll, with a three-band ratio being the best. The primary advantage of the three-band ratio was found to be its apparent insensitivity to atmospheric and Sun-angle variations.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-TM-84590 , L-15572 , NAS 1.15:84590
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    NASA TECHNICAL REPORTS
  • 9
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    Instrumental effects on the temperature and density derived from the light ion mass spectrometer (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: An expression for the flux into a retarding potential analyzer (RPA) is derived which takes into account the instrumental effect of a dependence on energy of the solid angle of the acceptance cone. A second instrumental effect of a limited bandpass is briefly discussed. Using the (LIMS) instrument on SCATHA, it is shown that temperatures and densities derived without considering the effect of the solid angle dependence on energy will be too low, dramatically so for E(t) E(1), where E(1) is the e folding distance of the solid angle dependence and E(t) is the thermal energy of the plasma. For E(t) E(1), there is effectively no impact on the derived temperatures and densities if the solid angle effect is ignored.
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
    Type: NASA-TM-82536 , NAS 1.15:82536
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    Analytical and Experimental Evaluation of the Heat Transfer Distribution over the Surfaces of Turbine Vanes (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Three airfoil data sets were selected for use in evaluating currently available analytical models for predicting airfoil surface heat transfer distributions in a 2-D flow field. Two additional airfoils, representative of highly loaded, low solidity airfoils currently being designed, were selected for cascade testing at simulated engine conditions. Some 2-D analytical methods were examined and a version of the STAN5 boundary layer code was chosen for modification. The final form of the method utilized a time dependent, transonic inviscid cascade code coupled to a modified version of the STAN5 boundary layer code featuring zero order turbulence modeling. The boundary layer code is structured to accommodate a full spectrum of empirical correlations addressing the coupled influences of pressure gradient, airfoil curvature, and free-stream turbulence on airfoil surface heat transfer distribution and boundary layer transitional behavior. Comparison of pedictions made with the model to the data base indicates a significant improvement in predictive capability.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-168015 , NAS 1.26:168015 , EDR-11209
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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