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  • COMPOSITE MATERIALS
  • Humans
  • 2000-2004
  • 1990-1994
  • 1980-1984  (2)
  • 1982  (2)
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  • 2000-2004
  • 1990-1994
  • 1980-1984  (2)
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  • 1
    Publication Date: 1982-07-23
    Description: Two families were studied in which the same homolog of chromosome pair 10 expressed both the fragile sites on the long (q) arm at 10q23 and 10q25. Recombination between the fragile sites was observed in 3 of the 27 offspring in whom it could occur. The genetic length of chromosome between the fragile sites was 11 female centimorgans within a 95 percent probability interval of 4 to 28 centimorgans. This estimate of genetic length is comparable to those obtained with other methods.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Sutherland, G R -- Baker, E -- Mulley, J C -- New York, N.Y. -- Science. 1982 Jul 23;217(4557):373-4.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/7089572" target="_blank"〉PubMed〈/a〉
    Keywords: Chromosome Banding ; Chromosome Fragile Sites ; *Chromosome Fragility ; Chromosome Mapping ; Chromosomes, Human, 6-12 and X/*ultrastructure ; Crossing Over, Genetic ; Female ; Humans ; Karyotyping ; Male ; Meiosis ; Pedigree ; Recombination, Genetic
    Print ISSN: 0036-8075
    Electronic ISSN: 1095-9203
    Topics: Biology , Chemistry and Pharmacology , Computer Science , Medicine , Natural Sciences in General , Physics
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  • 2
    Publication Date: 2019-06-28
    Description: Stress analysis of the Advanced Attack Helicopter (AAH) composite main rotor blade root end lug is described. The stress concentration factor determined from a finite element analysis is compared to an empirical value used in the lug design. The analysis and test data indicate that the stress concentration is primarily a function of configuration and independent of the range of material properties typical of Kevlar-49/epoxy and glass epoxy.
    Keywords: COMPOSITE MATERIALS
    Type: NASA-TM-84578 , NAS 1.15:84578
    Format: application/pdf
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