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  • 1
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    Tumor rejection after direct costimulation of CD8+ T cells by B7-transfected melanoma cells (1993)
    American Association for the Advancement of Science (AAAS)
    Details
    Publication Date: 1993-01-15
    Description: A variety of tumors are potentially immunogenic but do not stimulate an effective anti-tumor immune response in vivo. Tumors may be capable of delivering antigen-specific signals to T cells, but may not deliver the costimulatory signals necessary for full activation of T cells. Expression of the costimulatory ligand B7 on melanoma cells was found to induce the rejection of a murine melanoma in vivo. This rejection was mediated by CD8+ T cells; CD4+ T cells were not required. These results suggest that B7 expression renders tumor cells capable of effective antigen presentation, leading to their eradication in vivo.〈br /〉〈span class="detail_caption"〉Notes: 〈/span〉Townsend, S E -- Allison, J P -- CA57986/CA/NCI NIH HHS/ -- New York, N.Y. -- Science. 1993 Jan 15;259(5093):368-70.〈br /〉〈span class="detail_caption"〉Author address: 〈/span〉Department of Molecular and Cell Biology, University of California, Berkeley 94720.〈br /〉〈span class="detail_caption"〉Record origin:〈/span〉 〈a href="http://www.ncbi.nlm.nih.gov/pubmed/7678351" target="_blank"〉PubMed〈/a〉
    Keywords: Animals ; Antigen-Presenting Cells/immunology ; Antigens, CD80 ; Antigens, Surface/genetics/*immunology ; CD4-Positive T-Lymphocytes/immunology ; Cross Reactions ; Female ; Gene Expression Regulation ; Genetic Vectors ; Ligands ; *Lymphocyte Activation ; Melanoma/*immunology ; Mice ; Mice, Inbred BALB C ; Mice, Inbred C3H ; Mice, Nude ; T-Lymphocytes, Regulatory/*immunology ; Transfection ; Tumor Cells, Cultured
    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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    Turbomachinery CFD on parallel computers (1992)
    In:  Other Sources
    Details
    Publication Date: 2019-08-28
    Description: The role of multistage turbomachinery simulation in the development of propulsion system models is discussed. Particularly, the need for simulations with higher fidelity and faster turnaround time is highlighted. It is shown how such fast simulations can be used in engineering-oriented environments. The use of parallel processing to achieve the required turnaround times is discussed. Current work by several researchers in this area is summarized. Parallel turbomachinery CFD research at the NASA Lewis Research Center is then highlighted. These efforts are focused on implementing the average-passage turbomachinery model on MIMD, distributed memory parallel computers. Performance results are given for inviscid, single blade row and viscous, multistage applications on several parallel computers, including networked workstations.
    Keywords: COMPUTER SYSTEMS
    Type: Computing Systems in Engineering (ISSN 0956-0521); 3; 6; p. 613-623.
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Analysis of Inlet-Compressor Acoustic Interactions Using Coupled CFD Codes (1998)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: A problem that arises in the numerical simulation of supersonic inlets is the lack of a suitable boundary condition at the engine face. In this paper, a coupled approach, in which the inlet computation is coupled dynamically to a turbomachinery computation, is proposed as a means to overcome this problem. The specific application chosen for validation of this approach is the collapsing bump experiment performed at the University of Cincinnati. The computed results are found to be in reasonable agreement with experimental results. The coupled simulation results could also be used to aid development of a simplified boundary condition.
    Keywords: Aircraft Propulsion and Power
    Type: NASA/TM-1998-208839 , NAS 1.15:208839 , AIAA Paper 98-0749 , E-11451 , Aerospace Sciences; Jan 11, 1999 - Jan 14, 1999; Reno, NV; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Parallel NPARC: Implementation and Performance (1996)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Version 3 of the NPARC Navier-Stokes code includes support for large-grain (block level) parallelism using explicit message passing between a heterogeneous collection of computers. This capability has the potential for significant performance gains, depending upon the block data distribution. The parallel implementation uses a master/worker arrangement of processes. The master process assigns blocks to workers, controls worker actions, and provides remote file access for the workers. The processes communicate via explicit message passing using an interface library which provides portability to a number of message passing libraries, such as PVM (Parallel Virtual Machine). A Bourne shell script is used to simplify the task of selecting hosts, starting processes, retrieving remote files, and terminating a computation. This script also provides a simple form of fault tolerance. An analysis of the computational performance of NPARC is presented, using data sets from an F/A-18 inlet study and a Rocket Based Combined Cycle Engine analysis. Parallel speedup and overall computational efficiency were obtained for various NPARC run parameters on a cluster of IBM RS6000 workstations. The data show that although NPARC performance compares favorably with the estimated potential parallelism, typical data sets used with previous versions of NPARC will often need to be reblocked for optimum parallel performance. In one of the cases studied, reblocking increased peak parallel speedup from 3.2 to 11.8.
    Keywords: Aerodynamics
    Type: NASA-CR-202312 , NAS 1.26:202312 , E-10605 , AIAA Paper 97-0026 , Aerospace Sciences Meeting and Exhibit; Jan 06, 1997 - Jan 10, 1997; Reno, NV; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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