| Title | Author | Report Date | | Need for robust RF MEMS for space applications | Vendier, Olivier; Cazaux, J-L; Drevon, C; Cailloce, Y; Legay, H; Caille, G; Alcatel Space 26 av JF Champollion BP1187 31037 TOULOUSE CEDEX 1 - FRANCE | 2004 | | Wind Tunnel Test of an RPV with Shape-Change Control Effector and Sensor Arrays | Raney, David L; Cabell, Randolph H; Barnwell, William G; Lion, S Todd; Sloan, Adam R; Hautamaki, Bret A; NASA Langley Research Center | 2004 | | Three-dimensional effects on shock wave reflections in steady flows | Sudani, Norikazu^Sato, Mamoru^Watanabe, Mitsunori^Noda, Junichi^Tate, Atsushi^Karasawa, Toshio (National Aerospace Lab., Chofu, Japan) | | | Acoustic control of a rocket fairing using spatially weighted transducer arrays | Lane, Steven A. (Jackson and Tull Engineering, Albuquerque, NM)^Kemp, Jonathan D.^Clark, Robert L. (Duke Univ., Durham, NC)^Griffin, Steven F. (USAF, Research Lab., Kirtland AFB, NM) | | | A methodology for the design of APU air inlets for regional commercial aircraft | Jesus, Antonio (EMBRAER, Sao Jose dos Campos, Brazil)^Oliveira, Guilherme^Brodt, Claudio | 2002 | | Simultaneous optimization of design and manufacture of composite structures | Park, Chung Hae (Seoul National Univ., Republic of Korea; Saint-Etienne, Ecole Nationale Superieure des Mines, France)^Kim, Seung Jo^Lee, Woo Il (Seoul National Univ., Republic of Korea)^Han, Woo Suck^Vautrin, Alain (Saint-Etienne, Ecole Nationale Superieure des Mines, France) | | | Application of optimal control theory to turning control problem of vertical launching vessel-to-air missile | Tang, Shantong (Beijing Inst. of Electronics Systems Engineering, China) | | | Development of a strategic business decision-making environment for commercial jet engine selection | Mavris, Dimitri (Georgia Inst. of Technology, Atlanta)^Briceno, Simon^Fernandez, Ismael | 2002 | | Conurrent subsystem unertainty analysis in multidisiplinary design | Du, Xiaoping^Chen, Wei (Illinois, Univ., Chiago) | | | Performance prediction of experimental device of CUSP type direct energy converter | Kaminaga, Makoto^Ishikawa, Motoo (Tsukuba, Univ., Japan)^Mima, Suguru^Yasaka, Yasunori (Kyoto Univ., Japan)^Tomita, Yukihiro (National Inst. for Fusion Science, Toki, Japan)^Momota, Hiromu (NPL Associates, Champaign, IL) | | | Parametric Investigation of Combustion in Compressible Flows | Rusak, Zvi; Lee, Jang-Chang; Rensselaer Polytechnic Inst., Troy, NY | 2005 | | TURBULENT FLOW OVER A SPHERE WITH SUCTION AND BLOWING HOLES AND A GOLF BALL: A NUMERICAL STUDY | Alammar, Khalid N; King Saud University | 2004 | | Investigation of the combustion behaviour of solid fuel slabs in a planar step combustor with a colour Schlieren technique | Ciezki, Helmut K. (DLR, Hardthausen, Germany) | | | Optimizing hypersonic sharp body concepts from a thermal protection system perspective | Kolodziej, Paul^Bowles, Jeffery V. (NASA, Ames Research Center, Moffett Field, CA)^Roberts, Cathy (Sterling Software, Inc.; NASA, Ames Research Center, Moffett Field, CA) | | | Optimization of Bleed-Flow-Control for an Aggressive Serpentine Duct | Florea, Razvan; Haas, Martin; Hardin, Larry W; Lents, Charles E; Stucky, Mark B; United Technologies Research Center, East Hartford, CT | 2005 | | Estimating time of arrival in heavy weather conditions | Krozel, Jimmy (Seagull Technology, Inc., Los Gatos, CA)^Lee, Changkil^Mitchell, Joseph S. B. (New York, State Univ., Stony Brook) | | | Flow visualization on lower surfaces of waverider configurations at Mach 5.5 | Ohta, T.^Urano, A.^Miyagawa, T.^Matsuzaki, R. (Tokyo Metropolitan Inst. of Technology, Hino, Japan) | | | Disturbance accommodating spacecraft attitude control using thruster | Kim, Jinho^Kim, Jongrae (Inha Univ., Inchon, Republic of Korea) | | | Soot surface growth and oxidation in laminar unsaturated-hydrocarbon/air diffusion flames | El-Leathy, A. M. (Michigan, Univ., Ann Arbor)^Xu, F.^Faeth, G. M. | 2002 | | Nuclear propulsion system options for Mars missions | EMRICH, WILLIAM J., JR.^YOUNG, ARCHIE C. (NASA, Marshall Space Flight Center, Huntsville, AL) | | | Numerical simulation of a complete STOVL aircraft in ground effect | Smith, Merritt H.^Chawla, Kalpana^Van Dalsem, William R. (NASA, Ames Research Center, Moffett Field, CA) | | | The development of the ducted fan noise propagation and radiation code CDUCT-LaRC | Nark, Douglas M. (NASA, Langley Research Center, Hampton, VA)^Farassat, Fereidoun^Pope, D. Stuart^Vatsa, Veer | 2003 | | Missile Technology Demonstration 3 (MTD-3) demonstrating Global Positioning System (GPS) technology in an application to range safety tracking and precision guidance, navigation and control | Slivinsky, S.^Galloway, R.^Breitling, S. (USAF, Space Vehicles Directorate, Kirtland AFB, NM)^Wilborn, C. (Nichols Research Corp., Albuquerque, NM) | | | Attitude control system design for return of the Kistler K1 orbital vehicle | Rubinstein, David S.^Carter, David W. (Charles Stark Draper Lab., Inc., Cambridge, MA) | | | Sliding discharges for aerodynamics | Bychkov, V; Chernikov, V; Gromov, V; Levin, V; Shvets, A; Kuz'min, G; Minaev, I; Rukhadze, A; Timofeev, I; Lomonosov Moscow State Univ., Russia | 2005 |
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