Academic literature on the topic 'Aero optics'
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Journal articles on the topic "Aero optics"
Jumper, Eric J. "Special Section Guest Editorial: Aero-Optics and Adaptive Optics for Aero-Optics." Optical Engineering 52, no. 7 (April 15, 2013): 071401. http://dx.doi.org/10.1117/1.oe.52.7.071401.
Full textJumper, Eric J., Michael A. Zenk, Stanislav Gordeyev, David Cavalieri, and Matthew R. Whiteley. "Airborne Aero-Optics Laboratory." Optical Engineering 52, no. 7 (February 28, 2013): 071408. http://dx.doi.org/10.1117/1.oe.52.7.071408.
Full textJumper, Eric J., and Edward J. Fitzgerald. "Recent advances in aero-optics." Progress in Aerospace Sciences 37, no. 3 (April 2001): 299–339. http://dx.doi.org/10.1016/s0376-0421(01)00008-2.
Full textGoorskey, David J., Richard Drye, and Matthew R. Whiteley. "Dynamic modal analysis of transonic Airborne Aero-Optics Laboratory conformal window flight-test aero-optics." Optical Engineering 52, no. 7 (March 7, 2013): 071414. http://dx.doi.org/10.1117/1.oe.52.7.071414.
Full textSutton, George W., John E. Pond, Ronald Snow, and Yanfang Hwang. "Hypersonic interceptor aero-optics performance predictions." Journal of Spacecraft and Rockets 31, no. 4 (July 1994): 592–99. http://dx.doi.org/10.2514/3.26483.
Full textDe Lucca, Nicholas, Stanislav Gordeyev, and Eric Jumper. "In-flight aero-optics of turrets." Optical Engineering 52, no. 7 (January 31, 2013): 071405. http://dx.doi.org/10.1117/1.oe.52.7.071405.
Full textWang, Meng, Ali Mani, and Stanislav Gordeyev. "Physics and Computation of Aero-Optics." Annual Review of Fluid Mechanics 44, no. 1 (January 21, 2012): 299–321. http://dx.doi.org/10.1146/annurev-fluid-120710-101152.
Full textTrolinger, J. "New interferometry tools for aero-optics." Imaging Science Journal 59, no. 2 (April 2011): 113–26. http://dx.doi.org/10.1179/174313111x12966579709430.
Full textWang, Kan, and Meng Wang. "Aero-optics of subsonic turbulent boundary layers." Journal of Fluid Mechanics 696 (February 24, 2012): 122–51. http://dx.doi.org/10.1017/jfm.2012.11.
Full textYang Wenxia, 杨文霞, 蔡超 Cai Chao, 丁明跃 Ding Mingyue, and 周成平 Zhou Chengping. "Characterization of Aero-Optic Effects and Restoration of Aero-Optical Degraded Images." Acta Optica Sinica 29, no. 2 (2009): 347–52. http://dx.doi.org/10.3788/aos20092902.0347.
Full textDissertations / Theses on the topic "Aero optics"
Wang, Kan. "Computational investigation of aero-optical distortions by turbulent boundary layers and separated shear layers." Thesis, University of Notre Dame, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=3578995.
Full textAero-optical distortions are detrimental to airborne optical systems. To study distortion mechanisms, compressible large-eddy simulations are performed for a Mach 0.5 turbulent boundary layer and a separated shear layer over a cylindrical turret with and without passive control in the upstream boundary layer. Optical analysis is carried out using ray tracing based on the computed density field and Gladstone-Dale relation.
In the flat-plate boundary layer, the effects of aperture size, Reynolds number, small-scale turbulence, different flow regions and beam elevation angle are examined, and the underlying flow physics is analyzed. Three momemtum-thickness Reynolds numbers, Re&thetas; = 875, 1770 and 3550, are considered. It is found that the level of optical distortions decreases with increasing Reynolds number within the Reynolds number range considered. The contributions from the viscous sublayer and buffer layer are small, while the wake region plays a dominant role followed by the logarithmic layer. By low-pass filtering the fluctuating density field, it is shown that small-scale turbulence is optically inactive. Consistent with previous experimental findings, the distortion magnitude is dependent on the propagation direction due to anisotropy of the boundary-layer vortical structures. Density correlations and length scales are analyzed to understand the elevation-angle dependence and its relation to turbulence structures. The applicability of Sutton's linking equation to boundary-layer flows is examined, and excellent agreement between linking equation predictions and directly integrated distortions is obtained when the density length scale is appropriately defined.
The second case studied involves a separated shear layer over a cylindrical turret with a flat window, with inflow from a flat-plate boundary layer with and without passive control devices. The flow and optical results show reasonable agreement with experimental data for the baseline case without control. Aperture size effect, frequency spectra of OPD and two-point spatial correlations of OPD are investigated. The similarities and differences of distortion characteristics compared to those induced by turbulent boundary layers are discussed. The distortions by a separated shear layer are much larger in magnitude and spatially less homogeneous than those induced by an attached boundary layer. It is found that pressure fluctuations are significant and play a dominant role in inducing density fluctuations and associated optical distortions in a separated shear layer, in contrast to the dominant role of temperature fluctuations in a turbulent boundary layer. When passive control is applied using a row of thin and tall pins in the upstream boundary layer, the numerical results confirm key experimental findings. The flow above the optical window is characterized by two distinct shear layers, whose combined effect leads to a significant reduction of density fluctuation magnitude in the main shear layer and associated optical distortions compared to the uncontrolled flow with a single strong shear layer.
McGinnis, David C. "Aero Optic Characterization of Highly Turbulent Free Shear Layers Over a Backward Facing Step." University of Cincinnati / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1367928372.
Full textWillshire, Andrew J. "Robust optical sensor systems for aero-engine monitoring." Thesis, University of Strathclyde, 2004. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.423883.
Full textKelly, Ryan T. "Numerical prediction of the spatial and temporal characteristics of the aero-optical disturbance produced by a helicopter in hover." Thesis, University of Notre Dame, 2016. http://pqdtopen.proquest.com/#viewpdf?dispub=3746517.
Full textAero-optical disturbances produced from turbulent compressible flow-fields can seriously degrade the performance of an optical signal. At compressible flight speeds these disturbances stem from the density variations present in turbulent boundary layers and free shear layers; however helicopters typically operate at incompressible speeds, which nearly eliminates the aberrating effect of these flows. For helicopter platforms the sources of aberration originate from the high subsonic flow-field near the rotor blade tips in the form of rotor-tip vortices and from the high temperatures of the engine effluence. During hover the shed rotor-tip vortices and engine effluence convect with the rotor wake encircling the airframe and subsequently a helicopter mounted optical system.
The aero-optical effects of the wake beneath a hovering helicopter were analyzed using a combination of Unsteady RANS (URANS) and Large-Eddy Simulations (LES). The spatial and temporal characteristics of the numerical optical wavefronts were compared to full-scale aero-optic experimental measurements. The results indicate that the turbulence of the rotor-tip vortices contributes to the higher order aberrations measured experimentally and that the thermal exhaust plumes effectively limit the optical field-of-regard to forward- and side-looking beam directions. This information along with the computed optical aberrations of the wake can be used to guide the development of adaptive-optic systems or other beam-control approaches.
Arthington, Matthew Reginald. "Photogrammetric techniques for characterisation of anisotropic mechanical properties of Ti-6Al-4V." Thesis, University of Oxford, 2010. http://ora.ox.ac.uk/objects/uuid:51e4f4d9-75e2-4784-9fbf-103d07496e23.
Full textChang, Hsianglin, and 張祥琳. "Aero-Optics Analysis And Heat Insulation On An Optical Window Of A High Altitude Interceptor." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/58927755430967488440.
Full text國防大學理工學院
航空太空工程碩士班
100
In this study the simulation of forebody of interceptor through rarefied hypersonic gas flow at high altitude is taken for understanding the aerothermodynamic and aero-optic effects outside of the optical window. Wish to provide the reference data for the defense weapons R & D personnel. Research process is divided into the flow field simulation and the aero-optical analysis. First to obtain two-dimensional wedge oblique shock velocity by shock wave theory, then simplify the model into two-dimensional shallow cavity and use Direct Simulation Monte Carlo for simulation of flow field at different heights (60km, 80km, 100km). Subsequently jet flow is injected in the left side of the shallow cavity to simulate with the same conditions and compare the heat insulation effects of the jet. From the simulated flow field density distribution, the flow field can be simplified and roughly divided into three density interval. After individually derived its average density, the diplacement of image can be calculated from different incident angle (15°,30°, 45°,60°,75°) with Snell's Law and specific refractivity (Gladstone-Dale relation) for optical images analysis.
Tsai, Liang-Chih, and 蔡亮至. "Numerical Simulation of Aerodynamic Optical-Dome With Aero-Thermal Radiation Effect In Different Turbulence Models." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/02627558030510268519.
Full text國防大學理工學院
機械工程碩士班
100
The purpose of this study is to utilize CFD method to discuss under different turbulence models(DES、k-ε、k-ω) the hypersonic flow across the optical dome with cooling jets, the flow fields associated with geometry derived from the aerodynamic characteristics, the distribution of surface temperature combined with viscous dissipation and radiation effect of aerodynamic heating. Under such flow, due to the friction, the viscous effect near wall causesd no-slip codition, much of kinetic energy diffused to heat energy, hence, its surface and surrounding gases responded to temperature arised. By the cooling technology, the window cooled down against the heating load, meanwhile, the cooling jets would cause complicated shock and shock, shock and boundary interaction to affect flow field surrounding the window, additionally, the strong turbulent fluctuation and sheared effect while cooling jets mixed in main flow may lead to more complex disturbing between the flow properties of velocity, pressure, temperature and dentity to affect the result of real temperature, so we need to discuss in this study. The steady simulation of this study, the appropriate results of turbulence model compared to reference experimaental data of standoff distance validation is the k-ω. As thermal radiation effect introduced, the change of temperature at the stagnation point of nose would be 10.68% descent in DES turbulence model, 0.34% descent in k-ε model, and 6.31% in k-ω model. In order to make sure optical window temperature under 500K request, the optimum mass flow rate of cooling jets with dry air is 0.01kg/s. Further, under transient simulation without cooling, the during time of aerodynamic heating caused optical window’s surface temperature to reach critical temperature(500K) is 12 seconds for DES model, 10 seconds for k-ε model and 14 seconds for k-ω model.
Cross, Garnett B. "Investigation of a laser-induced breakdown spark as a near field guide star for aero-optic measurements." 2009. http://etd.nd.edu/ETD-db/theses/available/etd-12072009-130933/.
Full textThesis directed by R. Mark Rennie and Eric J. Jumper for the Department of Aerospace and Mechanical Engineering. "December 2009." Includes bibliographical references (leaves 62-64).
Lo, Tzu-Yi, and 羅子益. "Effect of Coolant Passage Configuration on the Film Cooling Performance of Aero-Optic Infra-Real Window with CFD Approach." Thesis, 2009. http://ndltd.ncl.edu.tw/handle/55205518479555994614.
Full text國防大學理工學院
機械工程碩士班
97
The aim of this thesis is to investigate the thermal protection performance of cooled slot flow over an IR optical window equipped in the head of a hypersonic flight missile with CFD method. The seeker in the IR window is used to track the target then to guide the missile to the modified trajectory in high flight speed. As the anti-missile vehicle flight in the high attitude atmosphere layer, most of the kinetic energy will be transformed into the thermal energy over the surfaces of missile body due to the thin shock layer characteristics. Therefore, the flow field nearby the IR window is influenced by the interaction of shock wave and developing boundary layer flow. The variations in density, pressure and species concentration result in high temperature gradient over the IR window. Not only the structure strength of IR window but also the aero-optic performance in such a severe environment must be considered in the design stage. To reduce the heat load on the IR window, the external film cooling method from a slot with various mass flow rates is used in present work. The numerical code is validated with similar cases in literatures before conducting runs. Three different types of cooled flow passage configuration were tested when the flight Mach number is 6. Results indicate that the optimum configuration is the forward inclined angle of 225 degree cavity model over tested ranges of mass flow rate of coolant. Comparison of .area-averaged film cooling performance among tested cases shows that the mass flow rate of 0.125 kg/s is suitable for cooling down the surface temperature of IR window below 500K. There is a minor influence of attack angle on the film cooling performance of slot flow over present IR window.
SHEN, JIN-LONG, and 沈金龍. "Aero-thermodynamic Analyses on Hypersonic Rarefied Flow over 3D Interceptor with Gas Coolant Jet of Optical Window." Thesis, 2017. http://ndltd.ncl.edu.tw/handle/u4r54y.
Full text國防大學理工學院
機械工程碩士班
105
Continual research efforts should be devoted in support of the development of hypersonic interceptor to provide protection against the threats of ballistic missiles. The infrared (IR) sensors system designed for targeting of hypersonic interceptor demand a very high precision detection. A viewing window must maintain its optical transparency to IR throughout the operational flight envelope. IR seekers on interceptors at high Mach number often suffer from degradation in performance due to aero-thermodynamic effects. This results in high heat, thermal radiation, and interference with image transmission in the seeker, leading to target image offsets, jitter, and fuzziness. It seems that cooling devices to protect optical window system may have to be provided. With the advancement of computational capability, the thermal response of the optical window induced by the hypersonic flow field can be evaluated through numerical calculations which simulate flight conditions as close as possible. In this study, the improved Direct Simulation Monte Carlo (DSMC) method is adopted to implement the three dimensional computations of the coolant jet of optical window flow field with hypersonic and rarefied conditions. The simulation results are expected to provide not only the better understanding of aero-thermal characteristics in the hypersonic three-dimensional fore-body flow but also useful information for practical design and improvement of the optical window system. In the study, we shall first construct a three dimensional grid system modeling the interceptor missile fore-body with optical window at high altitude of hypersonic rarefied gas flow field as shown. In order to effectively accelerate the overall computational efficiency, improved techniques such as variable time-step scheme, transient adaptive sub-cell method, the DSMC parallel processing, and proper gas-surface interaction models for wall boundary conditions will be employed. Simulation will be combined with unstructured mesh and message passing interface (MPI) of new parallel three dimensional DSMC code (PDSC++). Results indicate that the optimum configuration is the forward inclined angle of 45 degree cavity model over tested ranges of mass flow rate of coolant. Comparison of Nitrogen cooling performance among tested cases shows that velocity of 0.15m/s and the mass flow rate of 1.98188×10^22m^-3 is suitable for cooling down the surface temperature of window between 500K and 1200K.
Books on the topic "Aero optics"
Thomas, Bentley H., Society of Photo-optical Instrumentation Engineers., and University of Tennessee (System). Space Institute., eds. Flow visualization and aero-optics in simulated environments: 21-22 May 1987, Orlando, Florida. Bellingham, Wash., USA: SPIE, 1987.
Find full textGordeyev, Stanislav, Eric Jumper, and Matthew Whiteley. Aero-Optical Effects and Their Mitigation. Wiley & Sons, Incorporated, John, 2021.
Find full textGordeyev, Stanislav, Eric Jumper, and Matthew Whiteley. Aero-Optical Effects and Their Mitigation. Wiley & Sons, Incorporated, John, 2021.
Find full textUnited States. National Aeronautics and Space Administration., ed. MICRO-OPTICAL DISTRIBUTED SENSORS FOR AERO PROPULSION APPLICATIONS... NASA/CR--2003-212100... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. [S.l: s.n., 2003.
Find full textUnited States. National Aeronautics and Space Administration., ed. MICRO-OPTICAL DISTRIBUTED SENSORS FOR AERO PROPULSION APPLICATIONS... NASA/CR--2003-212100... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. [S.l: s.n., 2003.
Find full textUnited States. National Aeronautics and Space Administration., ed. MICRO-OPTICAL DISTRIBUTED SENSORS FOR AERO PROPULSION APPLICATIONS... NASA/CR--2003-212100... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. [S.l: s.n., 2003.
Find full textBook chapters on the topic "Aero optics"
Cassady, P. E., S. F. Birch, and P. J. Terry. "Aero-Optical Analysis of a Compressible Shear Layer." In Gas Flow and Chemical Lasers, 379–84. Berlin, Heidelberg: Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-71859-5_56.
Full textShi, Ketian, Jiatong Shi, and Handong Ma. "Aero-optical Effects Simulation Based on Turbulence Vortex Model." In Lecture Notes in Electrical Engineering, 2231–36. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_180.
Full textLee, Sangyoon, Man Chul Jeong, In-Seuck Jeung, Hyoung Jin Lee, and Jong Kook Lee. "Aero-Optical Measurement in Shock Wave of Hypersonic Flow Field." In 30th International Symposium on Shock Waves 1, 229–32. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_37.
Full textLee, Sangyoon, Hee Yoon, In-Seuck Jeung, Hyoung Jin Lee, and Jong Kook Lee. "Super-/Hypersonic Aero-Optical Effects Induced by External Jet Cooling." In 30th International Symposium on Shock Waves 1, 233–38. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_38.
Full textSchwingshackl, Christoph W. "Measuring Aero-Engine Pipe Vibration with a 3D Scanning Laser Doppler Vibrometer." In Rotating Machinery, Optical Methods & Scanning LDV Methods, Volume 6, 101–4. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-47721-9_11.
Full textKirmse, Tania, Anthony Gardner, and Christian Krombholz. "Investigation of Aero-Optical Effects in Model Deformation Measurements in a Transonic Flow." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 665–72. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-35680-3_79.
Full textHolden, M. S. "Ground Test Facilities and Instrumentation for Aerothermal and Aero-Optical Studies of Hypersonic Interceptors." In New Trends in Instrumentation for Hypersonic Research, 65–74. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1828-6_6.
Full textHarischandra, Najini, Nihal Kodikara, K. D. Sandaruwan, G. K. A. Dias, and Maheshya Weerasinghe. "Real-Time Simulation of Aero-optical Distortions Due to Air Density Fluctuations at Supersonic Speed." In Neural Information Processing, 653–62. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-26555-1_74.
Full textMafusire, Cosmas, and Andrew Forbes. "Aero - Optics: Controlling Light with Air." In Fluid Dynamics, Computational Modeling and Applications. InTech, 2012. http://dx.doi.org/10.5772/36643.
Full text"55. De aere et mutationibus eius." In Vocabularius optimus, 603–4. Max Niemeyer Verlag, 1990. http://dx.doi.org/10.1515/9783110923698.2.603.
Full textConference papers on the topic "Aero optics"
Sutton, George W., and John E. Pond. "Optics equations for aero-optical analysis." In International Conference on Applications of Optics and Photonics, edited by Manuel F. Costa. SPIE, 2011. http://dx.doi.org/10.1117/12.890265.
Full textSiegenthaler, John, Eric Jumper, and Stanislav Gordeyev. "Atmospheric Propagation vs. Aero-Optics." In 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-1076.
Full textClark, Rodney, Michele Banish, and Jay Hammer. "Fundamentals of aero-optics phenomena." In 25th Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2545.
Full textAbushagur, Mustafa A., and Ahmed Elmanasreh. "Aero-optics analysis using moire deflectometry." In Second Intl Conf on Photomechanics and Speckle Metrology: Moire Techniques, Holographic Interferometry, Optical NDT, and Applications to Fluid Mechanics. SPIE, 1991. http://dx.doi.org/10.1117/12.57501.
Full textGordeyev, Stanislav, Eric Jumper, and Tim Hayden. "Aero-Optics of Supersonic Boundary Layers." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-1325.
Full textHAVENER, GEORGE, and CHIP STEPANEK. "Aero-optics testing capabilities at AEDC." In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-760.
Full textPadé, Offer. "Modeling aero optics effects in jets." In SPIE Europe Security and Defence, edited by David H. Titterton and Mark A. Richardson. SPIE, 2008. http://dx.doi.org/10.1117/12.803568.
Full textJumper, Eric J., Mike Zenk, Stanislav Gordeyev, David Cavalieri, and Matthew R. Whiteley. "The Airborne Aero-Optics Laboratory, AAOL." In SPIE Defense, Security, and Sensing, edited by William E. Thompson and Paul F. McManamon. SPIE, 2012. http://dx.doi.org/10.1117/12.922734.
Full text"CFI-aero-optic images - Issues for wave optics modeling." In 25th Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2622.
Full textLADERMAN, A., W. MOTOOKA, and D. BARBER. "Aero/optics effects of airborne laser turrets." In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1397.
Full textReports on the topic "Aero optics"
Sherer, Scott E. Aero-Optics Code Development: Experimental Databases and AVUS Code Improvements. Fort Belvoir, VA: Defense Technical Information Center, March 2009. http://dx.doi.org/10.21236/ada501509.
Full textCoirier, William J., and James Stutts. Development of an Aero-Optics Software Library and Integration into Structured Overset and Unstructured Computational Fluid Dynamics (CFD) Flow Solvers. Fort Belvoir, VA: Defense Technical Information Center, April 2011. http://dx.doi.org/10.21236/ada547289.
Full textJumper, Eric J. Toward Adaptive Optic Mitigation of Aero-Optic Effects. Fort Belvoir, VA: Defense Technical Information Center, February 2009. http://dx.doi.org/10.21236/ada501712.
Full textOsher, Stanley, and Leonid Rudin. Feature-Oriented Image Reconstruction and Aero-Optic Metrology in Turbulence. Fort Belvoir, VA: Defense Technical Information Center, November 1994. http://dx.doi.org/10.21236/ada290269.
Full textSmits, A. J., and R. B. Miles. Shock Wave and Boundary Layer Control for Aero-Optic Application. Fort Belvoir, VA: Defense Technical Information Center, July 2002. http://dx.doi.org/10.21236/ada405454.
Full textJumper, Eric J., and R. M. Rennie. Aero-Optical Investigation of a Pod Directed Energy System. Fort Belvoir, VA: Defense Technical Information Center, February 2010. http://dx.doi.org/10.21236/ada517215.
Full textZilberter, Ilya A., and Jack R. Edwards. LES/RANS Modeling of Aero-Optical Effects in a Supersonic Cavity Flow. Fort Belvoir, VA: Defense Technical Information Center, June 2016. http://dx.doi.org/10.21236/ad1013250.
Full textThurow, Brian S. Yip - Development and Application of a High-Speed Three-Dimensional Density Measurement Technique for Aero-Optic Applications. Fort Belvoir, VA: Defense Technical Information Center, March 2011. http://dx.doi.org/10.21236/ada563707.
Full textLaFarge, R. A users' manual for MCPRAM (Monte Carlo PReprocessor for AMEER) and for the fuze options in AMEER (Aero Mechanical Equation Evaluation Routines). Office of Scientific and Technical Information (OSTI), May 1990. http://dx.doi.org/10.2172/6861389.
Full text