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  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (4)
  • EARTH RESOURCES AND REMOTE SENSING  (3)
  • Blood Flow Velocity  (1)
  • 1980-1984  (8)
  • 1975-1979
  • 1
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    Direct measurement of pulmonary capillary transit times (1982)
    American Association for the Advancement of Science (AAAS)
    Details
    Publication Date: 1982-10-22
    Description: Direct measurements of capillary transit times in dog lungs were made by using in vivo television microscopy. Mean transit times were unexpectedly long. As pulmonary artery pressures were raised, transit times decreased, suggesting that the normally existing hydrostatic pressure gradient in the lung causes a vertical distribution of transit times. The more rapid transit times approached the minimum time required for complete oxygenation.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Wagner, W W Jr -- Latham, L P -- Gillespie, M N -- Guenther, J P -- Capen, R L -- HL-07171/HL/NHLBI NIH HHS/ -- HL-14985/HL/NHLBI NIH HHS/ -- New York, N.Y. -- Science. 1982 Oct 22;218(4570):379-81.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/7123237" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Anoxia/physiopathology ; Blood Flow Velocity ; Blood Pressure ; Capillaries ; Dogs ; Lung/*blood supply ; Microscopy/methods ; Rheology
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
    Published by American Association for the Advancement of Science (AAAS)
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    PAPER CURRENT
  • 2
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    Heat capacity mapping mission project HCM-051 (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: There are no author-identified significant results in this report.
    Keywords: EARTH RESOURCES AND REMOTE SENSING
    Type: E80-10278 , NASA-CR-163344 , INTERNAL-TM-3/80
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    A NASTRAN model of a large flexible swing-wing bomber. Volume 4: NASTRAN model development-fuselage structure (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The NASTRAN model plan for the fuselage structure was expanded in detail to generate the NASTRAN model for this substructure. The grid point coordinates were coded for each element. The material properties and sizing data for each element were specified. The fuselage substructure model was thoroughly checked out for continuity, connectivity, and constraints. This substructure was processed for structural influence coefficients (SIC) point loadings and the deflections were compared to those computed for the aircraft detail model. Finally, a demonstration and validation processing of this substructure was accomplished using the NASTRAN finite element program. The bulk data deck, stiffness matrices, and SIC output data were delivered.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-170392-VOL-4 , NAS 1.26:170392-VOL-4 , NA-76-469-VOL-4
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    A NASTRAN model of a large flexible swing-wing bomber. Volume 5: NASTRAN model development-fairing structure (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The NASTRAN model plan for the fairing structure was expanded in detail to generate the NASTRAN model of this substructure. The grid point coordinates, element definitions, material properties, and sizing data for each element were specified. The fairing model was thoroughly checked out for continuity, connectivity, and constraints. The substructure was processed for structural influence coefficients (SIC) point loadings to determine the deflection characteristics of the fairing model. Finally, a demonstration and validation processing of this substructure was accomplished using the NASTRAN finite element program. The bulk data deck, stiffness matrices, and SIC output data were delivered.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-170392-VOL-5 , NAS 1.26:170392-VOL-5 , NA-76-469-VOL-5
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    A NASTRAN model of a large flexible swing-wing bomber. Volume 2: NASTRAN model development-horizontal stabilzer, vertical stabilizer and nacelle structures (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The NASTRAN model plans for the horizontal stabilizer, vertical stabilizer, and nacelle structure were expanded in detail to generate the NASTRAN model for each of these substructures. The grid point coordinates were coded for each element. The material properties and sizing data for each element were specified. Each substructure model was thoroughly checked out for continuity, connectivity, and constraints. These substructures were processed for structural influence coefficients (SIC) point loadings and the deflections were compared to those computed for the aircraft detail models. Finally, a demonstration and validation processing of these substructures was accomplished using the NASTRAN finite element program installed at NASA/DFRC facility.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-170392-VOL-2 , NAS 1.26:170392-VOL-2 , NA-76-469-VOL-2
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    A NASTRAN model of a large flexible swing-wing bomber. Volume 3: NASTRAN model development-wing structure (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The NASTRAN model plan for the wing structure was expanded in detail to generate the NASTRAN model for this substructure. The grid point coordinates were coded for each element. The material properties and sizing data for each element were specified. The wing substructure model was thoroughly checked out for continuity, connectivity, and constraints. This substructure was processed for structural influence coefficients (SIC) point loadings and the deflections were compared to those computed for the aircraft detail model. Finally, a demonstration and validation processing of this substructure was accomplished using the NASTRAN finite element program. The bulk data deck, stiffness matrices, and SIC output data were delivered.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-170392-VOL-3 , NAS 1.26:170392-VOL-3 , NA-76-469-VOL-3
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 7
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    High resolution satellite observations of mesoscale oceanography in the Tasman Sea, 1978 - 1979 (1982)
    In:  CASI
    Details
    Publication Date: 2019-07-20
    Description: Of the Nearly 1000 standard infrared photographic images received, 273 images were on computer compatible tape. It proved necessary to digitally enhance the scene contrast to cover only a select few degrees K over the photographic grey scale appropriate to the scene-specific range of sea surface temperature (SST). Some 178 images were so enhanced. Comparison with sea truth show that SST, as seen by satellite, provides a good guide to the ocean currents and eddies off East Australia, both in summer and winter. This is in contrast, particularly in summer, to SST mapped by surface survey, which usually lacks the necessary spatial resolution.
    Keywords: EARTH RESOURCES AND REMOTE SENSING
    Type: E82-10324 , NASA-CR-168903 , NAS 1.26:168903 , RANRL-1/82 , AR-002-695
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Heat Capacity Mapping Mission (1980)
    In:  CASI
    Details
    Publication Date: 2019-07-20
    Description: The Tasman Front was delineated by airborne expendable bathythermograph survey; and an Heat Capacity Mapping Mission (HCMM) IR image on the same day shows the same principal features as determined from ground-truth. It is clear that digital enhancement of HCMM images is necessary to map ocean surface temperatures and when done, the Tasman Front and other oceanographic features can be mapped by this method, even through considerable scattered cloud cover.
    Keywords: EARTH RESOURCES AND REMOTE SENSING
    Type: E81-10043 , NASA-CR-163753
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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