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  • 1
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    Histocompatibility and isoenzyme differences in commercially supplied "BALB/c" mice (1982)
    American Association for the Advancement of Science (AAAS)
    Details
    Publication Date: 1982-07-23
    Description: BALB/c mice obtained commercially were found to differ significantly from the standard phenotype of BALB/c strain mice. Isoenzyme tests and H-2 haplotype analyses indicated that the majority of mice from two of the three sources tested appeared mixed, frequently heterozygous, and did not consistently express either the expected H-2 or glucose phosphate isomerase type.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Kahan, B -- Auerbach, R -- Alter, B J -- Bach, F H -- New York, N.Y. -- Science. 1982 Jul 23;217(4557):379-81.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/6953593" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Cytotoxicity Tests, Immunologic ; Female ; Flow Cytometry ; Genetic Markers ; Glucose-6-Phosphate Isomerase/genetics ; H-2 Antigens/genetics/immunology ; Inbreeding ; Lymphocytes/immunology ; Male ; Mice ; Mice, Inbred BALB C/*genetics ; Phenotype
    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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  • 2
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    H-2 antigen class: effect on mouse islet allograft rejection (1983)
    American Association for the Advancement of Science (AAAS)
    Details
    Publication Date: 1983-03-18
    Description: Rejection of mouse pancreatic islet allografts occurred in a high percentage of donor recipient combinations identical for H-21-region antigens and differing at H-2K and H-2K + H-2D without I-region disparities. The results suggest that disparities in major histocompatibility complex antigens of class I (H-2K and H-2D) alone are capable of eliciting islet allograft rejection, and that lack of a stimulus from class II (I-region) alloantigens does not ensure permanent islet allograft survival.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Morrow, C E -- Sutherland, D E -- Steffes, M W -- Najarian, J S -- Bach, F H -- AI 18326/AI/NIAID NIH HHS/ -- AI/GM 17687/AI/NIAID NIH HHS/ -- AM 13083/AM/NIADDK NIH HHS/ -- etc. -- New York, N.Y. -- Science. 1983 Mar 18;219(4590):1337-9.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/6402817" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; *Graft Rejection ; H-2 Antigens/*immunology ; Histocompatibility Antigens Class II/*immunology ; *Islets of Langerhans Transplantation ; Major Histocompatibility Complex ; Mice ; T-Lymphocytes/immunology
    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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  • 3
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    Applications of state estimation in aircraft flight-data analysis (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: This paper traces the evolution of the use of state estimation in the analysis of aircraft flight data and discusses some recent applications associated with airline turbulence upsets and high-angle-of-attack flight tests. A unifying mathematical framework for state estimation is reviewed, and several examples are shown that illustrate a general approach for estimating variables that are difficult to measure. It is hoped that the diversity of the applications discussed and the examples presented will make the flight-data analyst mindful of the potential advantages of using state estimation methods.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 83-2087
    Format: text
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  • 4
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    A variational technique for smoothing flight-test and accident data (1980)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The problem of determining aircraft motions along a trajectory is solved using a variational algorithm that generates unmeasured states and forcing functions, and estimates instrument bias and scale-factor errors. The problem is formulated as a nonlinear fixed-interval smoothing problem, and is solved as a sequence of linear two-point boundary value problems, using a sweep method. The algorithm has been implemented for use in flight-test and accident analysis. Aircraft motions are assumed to be governed by a six-degree-of-freedom kinematic model; forcing functions consist of body accelerations and winds, and the measurement model includes aerodynamic and radar data. Examples of the determination of aircraft motions from typical flight-test and accident data are presented.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 80-1601 , Atmospheric Flight Mechanics Conference; Aug 11, 1980 - Aug 13, 1980; Danvers, MA
    Format: text
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    NASA TECHNICAL REPORTS
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