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  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE  (2)
  • Chemistry  (1)
  • Nutrients  (1)
  • 1975-1979  (4)
  • 1
    Electronic Resource
    Electronic Resource
    Preliminary observations on nitrogen transport during summer in a small spring-fed Ontario stream (1976)
    Springer
    Hydrobiologia 49 (1976), S. 59-63 
    Details
    ISSN: 1573-5117
    Keywords: Streams ; Nitrogen ; Nutrients ; Denitrification
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology
    Notes: Abstract Nitrogen transport in a 2 km-long, spring-fed stream was studied during the summer months by analyzing weekly water samples from four stations. The water at the spring had a consistently high level of nitrate-N ranging from about 7 mg/l in late spring to about 3 mg/l in early fall. However, over the length of the stream, 60% (about 97 kg) of the incoming nitrate-N is lost from the water during the summer period. The loss, which does not appear to be attributable to the uptake by aquatic macrophytes or to immobilization, is thought to result from denitrification.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1007/BF00016169
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    Paper (German National Licenses)
    Fulltext
  • 2
    Electronic Resource
    Electronic Resource
    Estimation of nitrogen-15 levels in derivatized amino acids using gas chromatography quadrupole mass spectrometry with chemical ionization and selected ion monitoringAbbreviation: HFBA = heptafluorobutyric anhydride. (1978)
    Chichester : Wiley-Blackwell
    Biological Mass Spectrometry 5 (1978), S. 648-653 
    Details
    ISSN: 0306-042X
    Keywords: Chemistry ; Analytical Chemistry and Spectroscopy
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: The data indicate that a commercial, low resolution mass spectrometer can be used with chemical ionization and selected ion monitoring, without a data system, to estimate nitrogen-15 isotopic enrichment with a sensitivity and precision adequate for many biological studies. This was demonstrated using derivatized amino acid mixtures with separation and direct introduction into the mass spectrometer via a gas chromatograph. The method can discriminate between mean levels separated by 0.1 atom % 15N with 68% confidence at the 0.1 nmol level. Labeled dansylamide samples, inserted by probe, were also measured for 15N content.
    Additional Material: 3 Ill.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/bms.1200051203
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    Paper (German National Licenses)
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  • 3
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    Unknown
    Application of an advanced computerized structural design system to an arrow-wing supersonic cruise aircraft (1975)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: A structural design study of an arrow-wing supersonic cruise aircraft has been made using the integrated design system, ATLAS, and a relatively large analytical finite-element model containing 8500 degrees of freedom. This paper focuses on structural design methods developed and used in support of the study with emphasis on aeroelasticity. The use of ATLAS permitted (1) automatic resizing of the wing structure for multiple load conditions, (2) rapid evaluation of aeroelastic effects, and (3) an iterative approach to the correction of flutter deficiencies. The significant results of the study are discussed along with the advantages derived from the use of an advanced structural design system in preliminary design studies.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 75-1038 , American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting; Aug 04, 1975 - Aug 07, 1975; Los Angeles, CA
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Unknown
    Design study of structural concepts for an arrow-wing supersonic-cruise aircraft (1975)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: An analytical study was performed to determine the best structural approach for design of primary wing and fuselage structure of a Mach number 2.7 arrow-wing supersonic cruise aircraft. Concepts were evaluated considering near-term start-of-design. Emphasis was placed on the complex interactions between thermal stress, static aeroelasticity, flutter, fatigue and fail-safe design, static and dynamic loads, and the effects of variations in structural arrangements, concepts and materials on these interactions. Results indicate that a hybrid wing structure incorporating low-profile convex-beaded and honeycomb sandwich surface panels of titanium alloy 6Al-4V were the most efficient. The substructure includes titanium alloy spar caps reinforced with Boron-polyimide composites. The fuselage shell is a closed-hat stiffened skin and frame construction of titanium alloy 6Al-4V. This paper presents an executive summary of the study effort, and includes a discussion of the overall study logic, design philosophy and interaction between the analytical methods for supersonic cruise aircraft design.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 75-1037 , American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting; Aug 04, 1975 - Aug 07, 1975; Los Angeles, CA
    Format: text
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    NASA TECHNICAL REPORTS
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