Relevant bibliographies by topics / NASP (Computer program)

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'NASP (Computer program)'

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Published: 4 June 2021
Last updated: 5 February 2022

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Journal articles on the topic "NASP (Computer program)"

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Semegni, J. Y., M. Wamalwa, R. Gaujoux, G. W. Harkins, A. Gray, and D. P. Martin. "NASP: a parallel program for identifying evolutionarily conserved nucleic acid secondary structures from nucleotide sequence alignments." Bioinformatics 27, no. 17 (2011): 2443–45. http://dx.doi.org/10.1093/bioinformatics/btr417.

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Brozowski, L. A., T. V. Ferguson, and L. Rojas. "Impeller Flow Field Laser Velocimeter Measurements." International Journal of Rotating Machinery 2, no. 3 (1996): 149–59. http://dx.doi.org/10.1155/s1023621x96000024.

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Development of Computational Fluid Dynamics (CFD) computer codes for complex turbomachinery affords a complete three-dimensional (3-D) flow field description. While significant improvements in CFD have been made due to improvements in computers, numerical algorithms, and physical modeling, a limited experimental database for pump CFD code validation exists.Under contract (NAS8-38864) to the National Aeronautics and Space Administration (NASA) at Marshall Space Flight Center (MSFC) a test program was undertaken at Rocketdyne to obtain benchmark data for typical rocket engine pump geometry. Noni
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Wade, R. A. "Synthetic Spectra for Accretion Discs: The UV Absorption Spectrum." International Astronomical Union Colloquium 158 (1996): 119–22. http://dx.doi.org/10.1017/s0252921100038409.

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With my collaborators (Ivan Hubeny, NASA/Goddard Space Flight Center; Marcos Diaz, Catherine Grant, and Darren Williams, all of Penn State), I am computing the structure of discs and their corresponding UV spectra for a large grid of choices of the white dwarf mass Mwd and the mass transfer rate Ṁ. In our approach, we divide the problem into a number of parts, each corresponding to a particular FORTRAN-implemented computer program. Program TLUSDISK computes the vertical structure for individual rings in the disc (T, ρ, ne, τ versus Z). The rings are treated independently, as plane-parallel ent
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Filipovic, Milos, and Nikola Kilibarda. "Calculation of complex chemical equilibrium compositions of composite rocket propellants combustion products." Journal of the Serbian Chemical Society 65, no. 11 (2000): 803–10. http://dx.doi.org/10.2298/jsc0011803f.

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An adequate method for calculating chemical equilibrium in a predominantly gaseous, multi-component reactive mixture was investigated and successfully applied. This method involves the stated equilibrium reaction scheme, including, first, the formation of chemical species, of which concentrations prevail in the mixture, then the formation of gaseous atomic species by dissociation of previous ones, and, finally, the formation of complex chemical species from the atomic species. A computer program, which permits calculations of equilibrium compositions by the iteration procedure, has been develo
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Rock, Donald A., and Jennifer Nelson. "Chapter 8: Applications and Extensions of NAEP Concepts and Technology." Journal of Educational Statistics 17, no. 2 (1992): 219–32. http://dx.doi.org/10.3102/10769986017002219.

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The National Assessment of Educational Progress (NAEP) has consistently pioneered new assessment methods in conjunction with developing the psychometric methodologies underlying them. Several NAEP developments—such as complex matrix item sampling designs, the introduction of performance-based items in large-scale assessments, vertical scaling, and an intelligent computer system that produces unique assessment reports for participating jurisdictions in the NAEP Trial State Assessment program—are presented in this chapter along with a discussion of their extensions and applications to other curr
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Abrams, Michael. "Retracing the Footprints." Mechanical Engineering 143, no. 3 (2021): 49–53. http://dx.doi.org/10.1115/1.2021-may4.

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Abstract NASA is engaged in a new program to send astronauts back to the lunar surface. Some elements of the new program, called Artemis, will seem like carbon copies of the 1960s roadmap to the Moon. Bu the effort will take advantage of computers, design tools, and materials that are radically more advanced than they were for the Apollo program.
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Fishbach, L. H., and S. Gordon. "NNEPEQ—Chemical Equilibrium Version of the Navy/NASA Engine Program." Journal of Engineering for Gas Turbines and Power 111, no. 1 (1989): 114–16. http://dx.doi.org/10.1115/1.3240205.

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The Navy NASA Engine Program, NNEP, developed in 1975, currently is in use at a large number of government agencies, commercial companies, and universities. This computer code has been used extensively to calculate the design and off-design (matched) performance of a broad range of turbine engines, ranging from subsonic turboprops to variable cycle engines for supersonic transports. Recently, there has been increased interest in applications that NNEP was not capable of simulating, namely, high Mach applications, alternate fuels including cryogenics, and cycles such as the gas generator air-tu
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Kotnour, Tim, and Timothy R. Bollo. "Strategic management of a transformation in a multi-program technology program involving convergence and divergence of programs: observations from NASA." International Journal of Technology Management 53, no. 2/3/4 (2011): 257. http://dx.doi.org/10.1504/ijtm.2011.038593.

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Inoue, K., D. P. Townsend, and J. J. Coy. "Optimum Design of a Gearbox for Low Vibration." Journal of Mechanical Design 115, no. 4 (1993): 1002–7. http://dx.doi.org/10.1115/1.2919247.

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A computer program was developed for designing a low vibration gearbox. The code is based on a finite element shell analysis, a modal analysis, and a structural optimization method. In the finite element analysis, a triangular shell element with 18 degrees-of-freedom is used. In the optimization method, the overall vibration energy of the gearbox is used as the objective function and is minimized at the exciting frequency by varying the finite element thickness. Modal analysis is used to derive the sensitivity of the vibration energy with respect to the design variable. The sensitivity is repr
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Yates, E. Carson. "Integral Equation Methods for Linear and Nonlinear Aerodynamics." Applied Mechanics Reviews 44, no. 11S (1991): S285—S294. http://dx.doi.org/10.1115/1.3121367.

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This paper reviews the NASA Langley Research Center program for development of integral-equation aerodynamic methods with emphasis on application in computed-aided multidisciplinary design processes as well as in aerodynamic design and stand-alone analysis. The accomplishments, status, and outlook of the program are discussed in order to highlight the scope, generality, versatility, and attractive features of this methodology, especially for application to nonlinear problems.
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Dissertations / Theses on the topic "NASP (Computer program)"

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Rosa, Harlei Vasconcelos. "Tecnologias digitais e educação : os dispositivos móveis nas políticas públicas de inserção das tecnologias na escola." Faculdade de Educação, 2017. http://repositorio.ufba.br/ri/handle/ri/23523.

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Submitted by Harlei Vasconcelos Rosa (harleivr@yahoo.com.br) on 2017-07-03T18:21:36Z No. of bitstreams: 1 TESE-HARLEI.pdf: 12166860 bytes, checksum: 528f3bc7b946339e6928da5aed268dab (MD5)<br>Approved for entry into archive by Maria Auxiliadora da Silva Lopes (silopes@ufba.br) on 2017-07-07T18:52:37Z (GMT) No. of bitstreams: 1 TESE-HARLEI.pdf: 12166860 bytes, checksum: 528f3bc7b946339e6928da5aed268dab (MD5)<br>Made available in DSpace on 2017-07-07T18:52:37Z (GMT). No. of bitstreams: 1 TESE-HARLEI.pdf: 12166860 bytes, checksum: 528f3bc7b946339e6928da5aed268dab (MD5)<br>Atualmente, as tecnologia
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Lasalvia, Vânia Cristina. "Análise do uso das tecnologias digitais nas escolas da região do médio São Francisco com foco no programa governamental Professor Conectado." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2017. http://hdl.handle.net/10183/172633.

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Pelo último censo realizado no ano de 2014 e divulgado no site da Secretaria de Educação de Pernambuco, o número de escolas da Rede Estadual de ensino básico chega a 1.052 escolas, que atendem aproximadamente 654 mil alunos e tem um quadro de 29.898 professores. Dessas escolas, 900 possuem internet e 732 escolas com banda larga. Existem 17.834 computadores distribuídos e instalados nesta rede de ensino dos quais, 3.430 para uso administrativo e 14.404 para uso dos alunos. No ano de 2008, o Governo de Pernambuco entregou notebook a todos os professores de regência da Rede. Em 2012 este Programa
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Abell, Barry J. "Planning concepts to sustain, develop, and test complex naval combat systems at the Surface Combat Systems Center, Wallops Island, Virginia." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Mar%5FAbell.pdf.

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Thesis (M.S. in Systems Engineering Management)--Naval Postgraduate School, March 2005.<br>Thesis Advisor(s): Scott Carlson, Benjamin Roberts. Includes bibliographical references (p. 145-152) Also available online.
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Books on the topic "NASP (Computer program)"

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Trosset, Michael W. Numerical optimization using computer experiments: NASA contract no. NAS1-19480. National Aeronautics and Space Administration, Langley Research Center, 1997.

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Wright, William B. User manual for the NASA Glenn Ice Accretion Code LEWICE. 2nd ed. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Roy, Daniel M. Ada projects at NASA: Runtime environment issues and recommendations. National Aeronautics and Space Administration, Goddard Space Flight Center, 1988.

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Brophy, Carolyn Elizabeth. Lessons learned in the transition from Ada to FORTRAN at NASA/Goddard. National Aeronautics and Space Administration, Goddard Space Flight Center, 1989.

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Gordon, Sanford. The NAVY/NASA Engine Program (NNEP89): Interfacing the Program for the calculation of Complex Chemical Equilibrium Compositions (CEC). National Aeronautics and Space Administration, 1991.

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Butrica, Andrew J. X-33 development history (contract NASW 97005): Progress report #4. National Aeronautics and Space Administration, 1997.

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Nguyen, L. Cathy. A users guide for the NASA ANOPP propeller analysis system. NASA Langley Research Center, 1997.

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Foltz, David A. Space Internet-Embedded Web Technologies demonstration. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Eichenlaub, Carl T. Using Penelope to assess the correctness of NASA Ada software: A demonstration of formal methods as a counterpart to testing. NASA, 1993.

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Justus, C. G. The NASA/MSFC global reference atmospheric model--1990 version (GRAM-90). School of Earth and Atmospheric Sciences, Georgia Institue of Technology, 1990.

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Book chapters on the topic "NASP (Computer program)"

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De Vos, Marina, and Dirk Vermeir. "Choice Logic Programs and Nash Equilibria in Strategic Games." In Computer Science Logic. Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/3-540-48168-0_19.

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Wong, Adam K. L., and Andrzej M. Goscinski. "Concurrent Execution of Multiple NAS Parallel Programs on a Cluster." In Lecture Notes in Computer Science. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/11428831_54.

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Cappello, Franck, Olivier Richard, and Daniel Etiemble. "Performance of the NAS Benchmarks on a Cluster of SMP PCs Using a Parallelization of the MPI Programs with OpenMP." In Lecture Notes in Computer Science. Springer Berlin Heidelberg, 1999. http://dx.doi.org/10.1007/3-540-48387-x_36.

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Daus, Yuliia, Valeriy Kharchenko, and Igor Viktorovich Yudaev. "Solar Radiation Intensity Data as Basis for Predicting Functioning Modes of Solar Power Plants." In Handbook of Research on Renewable Energy and Electric Resources for Sustainable Rural Development. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-3867-7.ch012.

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The chapter presents express methods for estimating the solar energy potential at a given point on the basis of combining the solar radiation daily profile application method under clear skies and actinometrical data of the NASA electronic base. Such a new approach including the climatological conditions of the region, significantly reduces the calculation time, and improves the accuracy of the decisions with a minimum of initial data. For the speed and convenience of calculations based on the proposed methodology, it was implemented in the form of a computer program. The article also analyzes the influence of spatial orientation on the maximum electricity produced during the month, season and year and it reveals that the use of an optimal inclination angle for the specified periods of time makes it possible to realize the existing solar potential of the region at the same capital expenditures.
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Herzig, Sebastian J. I., and Christiaan J. J. Paredis. "Probabilistic Reasoning and Inconsistency Identification in Graph-based Models." In Advances in Computers and Information in Engineering Research, Volume 2. ASME, 2021. http://dx.doi.org/10.1115/1.862025_ch17.

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In 1998, the National Aeronautics and Space Administration (NASA) launched the Mars Climate Orbiter (MCO) as part of the Mars Surveyor ’98 program. Upon arrival at Mars, MCO was to enter an elliptical orbit around the planet. On the day of orbit insertion, ground control was able to track the spacecraft visually up to the point when it vanished behind the planet. Unfortunately, the spacecraft never reappeared on the other side. It was later discovered that the probe came too close to the planet, and crashed into the Martian surface. The cause? A previously undiscovered mismatch in the use of unit systems for performing certain calculations in parts of the ground station software [43].
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Fisler, Kathi D. "Exploiting the Potential of Diagrams in Guiding Hardware Reasoning." In Logical Reasoning with Diagrams. Oxford University Press, 1996. http://dx.doi.org/10.1093/oso/9780195104271.003.0016.

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. . .Formal methods offer much more to computer science than just “proofs of correctness” for programs and digital circuits. Many of the problems in software and hardware design are due to imprecision, ambiguity, incompleteness, misunderstanding, and just plain mistakes in the statement of top-level requirements, in the description of intermediate designs, or in the specification of components and interfaces. Rushby [1993] . . .Desire for correctness proofs of systems spawned the research area known as “formal methods”. Today’s systems are of sufficient complexity that testing is infeasible, both computationally and financially. As an alternative, formal methods promote mathematical analysis of a system as a means of locating inconsistencies and other design errors. Techniques used can range from writing system descriptions in a formal notation to verification that the designed system satisfies a particular behavioral specification. A good general introduction to formal methods appears in Rushby [1993]. Ideally, using formal methods increases our assurance in and understanding of our designs. Assurance results from proof, while understanding results from the process of producing the proof. Successful use of formal methods therefore requires powerful proof techniques and clear logical notations. The verification research community has paid considerable attention to the former. Current techniques, many of which can be fully automated, handle sufficiently complex systems that formal methods are now being adopted (albeit slowly) in industry. In our drive to provide powerful proof methods, however, we have overlooked the latter requirement. Research has focused on proof without paying sufficient attention to reasoning. Current tools are often criticized as too hard to use, despite their computational power. Most designers, not having been trained as logicians, find the methodologies and notations very unnatural. Industrial sites, starting out with formal methods, must often rely on external verification professionals to help them use these tools effectively (NASA [1995]). Tools that are not supportive of reasoning therefore fail to provide the full benefits of formal methods. We can augment our current methodologies to address this problem, but we first need to understand reasoning and its role in hardware design.
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Bray, J., and G. Nana. "INTERNATIONAL ECONOMIC COORDINATION IN THE G7 AS A DYNAMIC NASH GAME11The model INTERMOD 1.1, a G7 version of the IMF model MULTIMOD model, was supplied by John Helliwell, Guy Meredith and Philip Bagnoli of the Department of Finance, Canada, with a simulation database. The Nash game algorithm and programme were supplied by the Programme for Research into Optimal Policy Evaluation (PROPE) at Imperial College, London (Elias Karakitsos, Berc Rustem, Robin Becker). These were embedded in the AMODEL simulation package supplied by the UK Treasury, and the whole installed in the Definicon/MS-DOS operating system environment of personal computers, by Sam Lovick." In Dynamic Modelling and Control of National Economies 1989. Elsevier, 1990. http://dx.doi.org/10.1016/b978-0-08-037538-0.50036-8.

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Conference papers on the topic "NASP (Computer program)"

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Powers, Lynn M., Alois Starlinger, and John P. Gyekenyesi. "Ceramic Component Reliability With the Restructured NASA/CARES Computer Program." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-383.

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The Ceramics Analysis and Reliability Evaluation of Structures (CARES) integrated design program on statistical fast fracture reliability of monolithic ceramic components is enhanced to include the use of a neutral data base, two-dimensional modeling and variable problem size. The data base allows for the efficient transfer of element stresses, temperatures and volumes/areas from the finite element output to the reliability analysis program. Elements are divided to insure a direct correspondence between the subelements and the Gaussian integration points. Two-dimensional modeling is accomplish
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Miller, Dean, Thomas Bond, David Sheldon, et al. "Validation of NASA thermal ice protection computer codes. I - Program overview." In 35th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-49.

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Yoshida, Makoto, Sazo Tsuruzono, Takashi Ono, and Hiroshi Gejima. "Development of Silicon Nitride Rotors for Gas Turbine Applications." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-332.

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Kyocera is developing various ceramic parts for gas turbines under the government funded ceramic gas turbine development programs in Japan. Among the programs, Kyocera is contracted for the development components for CGT-302 and CGT-303 engines which are designed for 300kW output power generation. Of the various parts for gas turbines, we discuss developments and burst tests at room temperature of silicon nitride turbine rotors made by slip casting. In particular, the result of burst tests of turbine rotors at room temperature is evaluated along with the strength prediction by a computer progr
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Inoue, Katsumi, Dennis P. Townsend, and John J. Coy. "Optimum Design of a Gearbox for Low Vibration." In ASME 1992 Design Technical Conferences. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/detc1992-0064.

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Abstract A computer program was developed for designing a low vibration gearbox. The code is based on a finite element shell analysis method, a modal analysis method, and a structural optimization method. In the finite element analysis, a triangular shell element with 18 degrees-of-freedom is used. In the optimization method, the overall vibration energy of the gearbox is used as the objective function and is minimized at the exciting frequency by varying the finite element thickness. Modal analysis is used to derive the sensitivity of the vibration energy with respect to the design variable.
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Lu, P. C., and Chen-Ying Wang. "AXITURB: A Full Computer Implementation of the NASA Design Procedure for Axial-Flow Turbines." In ASME 1993 International Computers in Engineering Conference and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/cie1993-0025.

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Abstract A recent task to design a Rankine-cycle space-power turbine system employing eutectic alloys of alkali metals prompted the present authors to re-examine the NASA design procedure for axial-flow turbines, as outlined by Glassman and Futral (and based on works of Stewart) in 1963. After clarifying the role of the singular case of a single-stage turbine, and organizing the procedure in clear steps, a computer program AXITURB was written. The present paper reports essentially the success of AXITURB in performing parametric studies of NaK and CsK turbines (using 78.4% and 23.1%, respective
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Jones, Kennie H., Donald P. Randall, Lawrence F. Rowell, Raymond L. Gates, Chris M. Nichols, and S. Blake Williams. "Environment for Application Software Integration and Execution." In ASME 1992 International Computers in Engineering Conference and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/edm1992-0142.

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Abstract The Environment For Application Software Integration and Execution (EASIE) is a methodology and a set of software utility programs developed at the NASA Langley Research Center for coordinating the use of engineering design and analysis computer programs. Under user direction, EASIE controls the execution of independently developed programs and manages the flow of data to and from a common relational data base in order to accomplish design or analysis objectives. The process is highly automated. For example, a utility program generates a DATA DICTIONARY, describing the contents of the
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Wan, S. M., T. C. T. Lam, J. M. Allen, and T. H. McCloskey. "A Gas Turbine Blade Thermal/Structural Program With Linked Flow-Solid Modeling Capability." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-270.

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A time-marching approach is adopted in developing a thermal/structural program with linked flow-solid modeling capability. The Blade Life Analysis &amp; Design Evaluation for Combustion Turbines (BLADE-CT) program analyzes gas turbine blade thermal-mechanical stress and natural frequencies under the boundary conditions which result from the gas flow and the cooling/barrier flow within a given turbine stage. Using the finite element method, the blade temperatures obtained from transient/steady-state thermal solutions can be utilized to compute thermal stresses and dynamic stresses under operati
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He, Chunlei, Sangbum Choi, D. Mirmirani, and Chivey Wu. "CFD-Based Aeroelastic Analysis in Transonic Flow Regime." In ASME 2004 International Mechanical Engineering Congress and Exposition. ASMEDC, 2004. http://dx.doi.org/10.1115/imece2004-61311.

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The aeroelastic instability behavior of the AGARD445.6 wing at transonic flight speed is investigated by using Finite Element-based unsteady CFD simulations and automated three-dimensional unstructured meshing. A general-purpose multidisciplinary computer program called STARS (Structural Analysis RoutineS), developed at NASA Dryden Flight Research Center is employed as the tool for this study. The computational results on flutter boundaries of the wing structure are compared with wind tunnel data, and have been found to be satisfactory.
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Burcham, Frank W., Timothy R. Conners, and Michael D. Maxwell. "Flight Research Using F100 Engine P680063 in the NASA F-15 Airplane." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-119.

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The value of flight research in developing and evaluating gas turbine engines is high. NASA Dryden Flight Research Center has been conducting flight research on propulsion systems for many years. The F100 engine has been tested in the NASA F-15 research airplane in the last three decades. One engine in particular, S/N P680063, has been used for the entire program and has been flown in many pioneering propulsion flight research activities. Included are detailed flight-to-ground facility tests; tests of the first production digital engine control system, the first active stall margin control sys
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McGlothlin, J., and D. Kings. "98. Evaluation and Validation of an Internet-Based Office Ergonomics Software Program for Correcting Computer Workstation Layout among Nasa Employees." In AIHce 2001. AIHA, 2001. http://dx.doi.org/10.3320/1.2766011.

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