| Title | Author | Report Date | | Applications of a highly efficient numerical method for overset-mesh moving body problems | Nichols, R. H. (Sverdrup Technology, Inc., AEDC Group, Arnold AFB, TN)^Tramel, R. W. (Micro Craft, Inc., Tullahoma, TN) | | | Simulation of chemically reacting flowfields around generic ASTV configuration including the wake | Gallis, M. A.^Harvey, J. K. (Imperial College of Science, Technology and Medicine, London, United Kingdom) | | | On methane combustion in a nozzle geometry using a reduced reaction kinetics model | Ingram, D. M.^Jiang, B.^Causon, D. M. (Manchester Metropolitan Univ., United Kingdom) | | | Proessing of arbon nanotubes for revolutionary spae appliations | Files, Bradley S. (NASA, Johnson Spae Center, Houston, TX) | | | Benefits of advanced structures technology in subsonic propulsion systems | Abumeri, Galib H. (NYMA, Inc., Brook Park, OH)^Chamis, Christos C. (NASA, Lewis Research Center, Cleveland, OH) | | | Fundamental physics utilizing laser-cooled atoms in microgravity | Thompson, R. J.^Seidel, D. J.^Klipstein, W. M.^Kohel, J.^Maleki, L. (JPL, Pasadena, CA) | 2001 | | Neural Network Model of Airbus A340 Flight Dynamics for Reliability Analyses | Demirci, Seref; Aykan, Rahmi; Turkish Airlines Inc., Yesilkoy, Istanbul, Turkey, 34850 | 2005 | | Adaptive asymptotic tracking of spacecraft attitude motion with inertia matrix identification | Ahmed, Jasim^Coppola, Vincent T.^Bernstein, Dennis S. (Michigan, Univ., Ann Arbor) | | | Output feedback form and adaptive control of a nonlinear aeroelastic system | Singh, Sahjendra (Nevada, Univ., Las Vegas)^Wang, Ling (Nevada, Univ., Las Vegas) | 2002 | | Validation of NASA thermal ice protection computer codes. I - Program overview | Miller, Dean^Bond, Thomas^Sheldon, David (NASA, Lewis Research Center, Cleveland, OH)^Wright, William^Langhals, Tammy (NYMA, Inc., Brook Park, OH)^Al-Khalil, Kamel (Cox & Co., Inc., New York)^Broughton, Howard (Cortez III Service Corp., Cleveland, OH) | | | Effective control of computationally simulated wing rock in subsonic flow | Kandil, Osama A.^Menzies, Margaret A. (Old Dominion Univ., Norfolk, VA) | | | Development of an object-oriented three-dimensional Burnett equations solver for computing hypersonic flows in continuum-transition regime | Swargam, Satish^Agarwal, Ramesh K.^Yun, Keon-Young (National Inst. for Aviation Research, Wichita, KS) | | | Tow-Placement Technology and Fabrication Issues for Laminated Composite Structures | Guerdal, Zafer; Tatting, Brian F; Wu, K Chauncey; Delft Univ. of Technology, Netherlands | 2005 | | Advanced nozzle and engine components test facility | BELTRAN, LUIS R.^DEL ROSO, RICHARD L.^DEL ROSARIO, RUBEN (NASA, Lewis Research Center, Cleveland, OH) | | | A high speed surface reflective visualization system for the study of vortex breakdown over a delta wing | Donohoe, S. R.^Houtman, E. M.^Bannink, W. J. (Delft Univ. of Technology, Netherlands) | | | Stage Analysis of Centrifugal Compressors for Design: CFD Validation | Srivastava, B N; Macrorie, M; Machnaim, J; General Electric Company | 2004 | | Recent developments in high efficiency, elastically deployed boom structures | Warren, Peter A. (Foster Miller, Inc., Waltham, MA)^Hinkle, Jason D.^Harvey, T. Jeff | 2003 | | Integrated flight/propulsion control specifications - Accounting for two-way coupling | Neighbors, W. K., III^Rock, Stephen M. (Stanford Univ., CA) | | | Determination of Strain Rate Dependent Compressive Strengths of Carbon Fiber Composites | Bing, Qida; Sun, C T; Purdue Univ., West Lafayette, IN | 2005 | | Accurate solution algorithms for incompressible multiphase flows | Rider, William J.^Kothe, Douglas B.^Mosso, S. J.^Cerutti, John H. (Los Alamos National Lab., NM)^Hochstein, John I. (Memphis State Univ., TN) | | | Model identification of a Kulite pressure transducer | Rotea, Mario A.^Randall, Laura A.^Song, Ge^Schneider, Steven P. (Purdue Univ., West Lafayette, IN) | | | Liquid and slush hydrogen ground support facilities for aero-space planes | BUTLER, DAVID A.^MOORE, ROBERT B. (Air Products and Chemicals, Inc., Allentown, PA) | | | Integrated control-structure design of the JPL phase B testbed | MILMAN, M.^SALAMA, M.^CHU, C. C.^WETTE, M. (JPL, Pasadena, CA) | | | Determining design gust loads for nonlinear aircraft similarity between methods based on matched filter theory and on stochastic simulation | SCOTT, ROBERT C. (NASA, Langley Research Center, Hampton, VA)^POTOTZKY, ANTHONY S. (Lockheed Engineering and Sciences Co., Hampton, VA)^PERRY, BOYD, III (NASA, Langley Research Center, Hampton, VA) | | | Viscous unstructured three-dimensional grids by the advancing-layers method | Pirzadeh, Shahyar (Vigyan, Inc., Hampton, VA) | |
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