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  • 1
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: Differentiation of the megakaryocytic leukemia cells, CMK, was induced by long-term (12 day) treatment with the combination of IL-3 and the nucleoside analogue ribavirin (RV), which reduces cellular GTP levels. In a previous report we demonstrated the induction of early messages and antigens, as well as the formation of giant polyploid cells in the cultures (Majumdar et al., 1994, J. Cell. Physiol., 160:29-39). Here we show high level induction of messages for the late markers, Platelet Factor 4, GMP140 (P-Selectin), thrombospondin, and beta thromboglobulin. The induced cells are also positive for these antigens by immunocytochemical analysis. The high level message induction resulted from synergy between the inducers. Pretreatment of the cells with IL-3 could accelerate the rise in message seen with the inducer combination. The increase in differentiation markers was accompanied by a reduction of the proliferative capacity of the cells. Riboguanosine, which has anti differentiation activity, blocked the induction of early and late antigens by the inducer combination, and also by IL-3 acting alone, but did not block the reduction in proliferative competence. In this model of megakaryocytic differentiation IL-3 treatment yields and initial stimulation of growth followed by growth supperssion, and is the principal driver of the differentiation process. RV functions primarily as a stimulator of message and protein expression in synergy with IL-3. © 1995 Wiley-Liss Inc.
    Additional Material: 7 Ill.
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  • 2
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: Megakaryocyte differentiation is a lengthy process with cells moving through a continuum delineated by the sequential expression of specific gene products. The limited number of primary cells available from marrow for analysis has brought attention to some leukemic cell lines which show enhanced megakaryocyte marker expression following incubation with inducing agents, the most common of which is phorbol myristate acetate (PMA). We developed an alternative induction protocol for the megakaryocytic leukemic cell line CMK, which involved incubation of the cells with IL-3 and the nucleoside analog, ribavirin, for 1-2 weeks. This treatment was neither toxic nor cytostatic and yielded increased levels of the surface glycoproteins GPIIb/IIIA and GPIb-IX. Levels of some megakaryocytic messages (GPIIIa, GPIX) showed a marked rise by 12 days of incubation in the inducer combination. This was due to a synergistic interaction between IL-3 and ribavirin which influenced both transcriptional and posttranscriptional events. Light and electron microscopy demonstrated the presence of large polyploid cells, with morphological features similar to those of megakaryocytes, in the induced cultures. Analysis of the heterogeneity of response in the cell population to the induction regimen after several days of treatment suggested that cells which failed to display surface markers had been stimulated by the inducers but did not have sufficient time to complete expression of that marker. The results were consistent with the view that the cells in the starting population were distributed along a temporal expression pathway, and those which were first to express the earliest marker would also lead in the expression of a later marker. The order of expression was the same as that during normal megakaryocyte development. © 1994 Wiley-Liss, Inc.
    Additional Material: 9 Ill.
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  • 3
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: The bone marrow microenvironment consists of stromal cells and extracellular matrix components which act in concert to regulate the growth and differentiation of hematopoietic stem cells. There is little understanding of the mechanisms which modulate the regulatory role of stromal cells. This study examined the hypothesis that mesenchymal growth factors such as basic fibroblast growth factor (bFGF) and epidermal growth factor (EGF) modulate stromal cell activities and thereby influence the course of hematopoiesis. Both bFGF and EGF were potent mitogens for marrow stroma. However, both factors proved to be inhibitory to hematopoiesis in primary log-term marrow cultures. Inhibition was also observed when hematopoietic cells and bFGF or EGF were added to subconfluent irradiated stromal layers, demonstrating that the decline of hematopoiesis was not due to overgrowth of the stromal layer. Loss of hematopoietic support in bFGF and EGF was dose-dependent. Removal of bFGF and EGF permitted stromal layers to regain their normal capacity to support hematopoiesis. In stroma-free long-term cultures, neither factor affected CFU-GM expansion. Basic FGF slightly enhanced granulocyte-macrophage colony forming unit (CFU-GM) cloning efficiency in short-term agarose culture. Basic FGF did not reduce the levels of interleukin-6 (IL-6), GM-CSF, or G-CSF released by steady state or IL-1-stimulated stroma. Similarly, the constitutive levels of steel factor (SF) mRNA and protein were not affected by bFGF. Basic FGF did not alter the level of TGF-β1 in stromal cultures. We conclude that bFGF and EGF can act as indirect negative modulators of hematopoietic growth in stromal cultures. The actual mediators of regulation, whether bound or soluble, remain to be identified. © 1995 Wiley-Liss, Inc.
    Additional Material: 13 Ill.
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  • 4
    Publication Date: 2018-06-05
    Description: The turbulent boundary layer (TBL) pressure field is an important source of cabin noise during cruise of high subsonic and supersonic commercial aircraft. The broadband character of this excitation field results in an interior noise spectrum that dominates the overall sound pressure level (SPL) and speech interference metrics in the forward and midcabins of many aircraft. In the authors' previous study, sound transmission through an aircraft fuselage, modeled by two concentric cylindrical sandwich shells and excited by a TBL statistical model was investigated analytically. An assessment of point and global structural vibration levels and resulting interior noise levels was obtained for different TBL models, flight conditions and fuselage structural designs. However, due to the complication of the shell structure, the important noise transmission mechanisms were difficult to discern. Previous experience has demonstrated that a fundamental understanding of the range of modes (or wavenumbers) generated by the TBL source both in the structure and the acoustic cavity is key to the development of both active and passive control technologies. In an initial effort to provide this insight, the objective of this paper is to develop an analytical model of sound transmission through a simple unstiffened cylindrical aluminum shell excited by a TBL pressure field. The description of the turbulent pressure field is based on the Corcos formulation for the cross-spectral density (CSD) of the pressure fluctuations. The coupled shell and interior and exterior acoustic equations are solved for the structural displacement and the interior acoustic response using a Galerkin approach to obtain analytical solutions. Specifically, this study compares the real part of the normalized CSD of the TBL excitation field, the structural displacement and the interior acoustic field. Further the modal compositions of the structural and cavity response are examined and some inference of the dominant mechanism of noise transmission is made.
    Keywords: Aircraft Design, Testing and Performance
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  • 5
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    In:  CASI
    Publication Date: 2019-07-27
    Description: The X-33 flight visualization effort has resulted in the integration of high-resolution terrain data with vehicle position and attitude data for planned flights of the X-33 vehicle from its launch site at Edwards AFB, California, to landings at Michael Army Air Field, Utah, and Maelstrom AFB, Montana. Video and Web Site representations of these flight visualizations were produced. In addition, a totally new module was developed to control viewpoints in real-time using a joystick input. Efforts have been initiated, and are presently being continued, for real-time flight coverage visualizations using the data streams from the X-33 vehicle flights. The flight visualizations that have resulted thus far give convincing support to the expectation that the flights of the X-33 will be exciting and significant space flight milestones... flights of this nation's one-half scale predecessor to its first single-stage-to-orbit, fully-reusable launch vehicle system.
    Keywords: Aircraft Design, Testing and Performance
    Type: Space Technology and Applications International Forum (STAIF); 31 Jan. 4 Feb. 1999; Albuquerque, NM; United States
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  • 6
    Publication Date: 2019-07-13
    Description: The validation of finite element and boundary element model for the vibro-acoustic response of a curved honeycomb core composite aircraft panel is completed. The finite element and boundary element models were previously validated separately. This validation process was hampered significantly by the method in which the panel was installed in the test facility. The fixture used was made primarily of fiberboard and the panel was held in a groove in the fiberboard by a compression fitting made of plastic tubing. The validated model is intended to be used to evaluate noise reduction concepts from both an experimental and analytic basis simultaneously. An initial parametric study of the influence of core thickness on the radiated sound power from this panel, using this numerical model was subsequently conducted. This study was significantly influenced by the presence of strong boundary condition effects but indicated that the radiated sound power from this panel was insensitive to core thickness primarily due to the offsetting effects of added mass and added stiffness in the frequency range investigated.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper 2003-3156 , 9th AIAA/CEAS Aeroacoustics Conference and Exhibition; May 12, 2003 - May 14, 2003; Hilton Head, SC; United States
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  • 7
    Publication Date: 2019-07-13
    Description: Supersonic aircraft designers must shape the outer mold line of the aircraft to improve multiple objectives, such as mission performance, cruise efficiency, and sonic-boom signatures. Conceptual designers have demonstrated an ability to assess these objectives for a large number of candidate designs. Other critical objectives and constraints, such as weight, fuel volume, aeroelastic effects, and structural soundness, are more difficult to address during the conceptual design process. The present research adds both static structural analysis and sizing to an existing conceptual design framework. The ultimate goal is to include structural analysis in the multidisciplinary optimization of a supersonic aircraft. Progress towards that goal is discussed and demonstrated.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper-2012-1753 , NF1676L-13121 , 53rd Structures, Structural Dynamics and Materials Conference; Apr 23, 2012 - Apr 26, 2012; Honolulu, HI; United States
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  • 8
    Publication Date: 2019-07-13
    Description: Composite structures are often used in aircraft because of the advantages offered by a high strength to weight ratio. However, the acoustical properties of these light and stiff structures can often be less than desirable resulting in high aircraft interior noise levels. In this paper, measurements and predictions of the transmission loss of a curved honeycomb composite panel are presented. The transmission loss predictions are validated by comparisons to measurements. An assessment of the behavior of the panel is made from the dispersion characteristics of transverse waves propagating in the panel. The speed of transverse waves propagating in the panel is found to be sonic or supersonic over the frequency range from 100 to 5000 Hz. The acoustical benefit of reducing the wave speed for transverse vibration is demonstrated.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper 2003-3157 , 9th AIAA/CEAS Aeroacoustics Conference and Exhibition; May 12, 2003 - May 14, 2003; Hilton Head, SC; United States
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