Books on the topic 'Supersonic nozzle'
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Scallion, W. I. Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textScallion, W. I. Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air. National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textRaman, Ganesh. The flip-flop nozzle extended to supersonic flows. National Aeronautics and Space Administration, 1992.
Find full textMichael, Hailye, Rice Edward J, and United States. National Aeronautics and Space Administration., eds. The flip-flop nozzle extended to supersonic flows. National Aeronautics and Space Administration, 1992.
Find full textRaman, Ganesh. The flip-flop nozzle extended to supersonic flows. National Aeronautics and Space Administration, 1992.
Find full textEhud, Gartenberg, Roberts A. Sidney, and Langley Research Center, eds. Investigation of ramp injectors for supersonic mixing enhancement. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textE, Gartenberg, Roberts A. S, and Langley Research Center, eds. Investigation of ramp injectors for supersonic mixing enhancement. National Aeronautics and Space Administration, Langley Research Center, 1994.
Find full textDash, Sanford M. Computational models for the analysis/design of hypersonic scramjet nozzles - Part 1: Combustor and nozzle models. AIAA, 1986.
Find full textMurthy, S. N. B. Analysis of supersonic plug nozzle flowfield and heat transfer. National Aeronautics and Space Administration, 1989.
Find full textSchneider, Steven P. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research: Final report. National Aeronautics and Space Administration, 1994.
Find full textKim, Y. N. Numerical analysis of some supersonic viscous flows related to inlet and nozzle systems. AIAA, 1986.
Find full textSchneider, Steven P. Method of characteristics design of a supersonic wind tunnel nozzle with square cross-section: Status report for NASA Langley grant NAG-1-113, supplement 3. National Aeronautics and Space Administration, 1993.
Find full textHao, Shen, Raman Ganesh, and United States. National Aeronautics and Space Administration., eds. Screech tones of supersonic jets from bevelled rectangular nozzles. American Institute of Aeronautics and Astronautics, 1997.
Find full textAbbas, Khavaran, Das A. P, and United States. National Aeronautics and Space Administration., eds. Computational noise study of a supersonic short conical plug-nozzle jet. National Aeronautics & Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. MCAT Institute, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. MCAT Institute, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. MCAT Institute, 1991.
Find full textRaman, Ganesh. Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle. National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle: Final report. MCAT Institute, 1995.
Find full textM, Seiner John, Brown Martha C, and Langley Research Center, eds. Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textL, Burstadt Paul, and United States. National Aeronautics and Space Administration., eds. Experimental results for a two-dimensional supersonic inlet used as a thrust deflecting nozzle. National Aeronautics and Space Administration, 1989.
Find full textBaysal, Oktay. Viscous computations of cold air/airflow around scramjet nozzle afterbody. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textGanesh, Raman, and United States. National Aeronautics and Space Administration., eds. Mixing noise reduction for rectangular supersonic jets by nozzle shaping and induced screech mixing. National Aeronautics and Space Administration, 1993.
Find full textBaysal, Oktay. Viscous computations of cold air/air flow around scramjet nozzle afterbody. Langley Research Center, 1991.
Find full textE, Beckwith Ivan, Chen Fang-Jenq, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textE, Beckwith Ivan, Chen Fang-Jenq, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textJ, Georgiadis Nicholas, and NASA Glenn Research Center, eds. An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textDembowski, Mary Ann. An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code. National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textCenter, Lewis Research, ed. Collective interaction in a linear array of supersonic rectangular jets: A linear spatial instability study. National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textSchneider, Steven P. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Supersonic quiet-tunnel development for laminar-turbulent transition research: Final report for NASA Langley grant NAG-1-1607. National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. A first scramjet study. National Aeronautics and Space Administration, 1989.
Find full textK, Ahuja K., and United States. National Aeronautics and Space Administration., eds. Shear flow control of cold and heated rectangular jets by mechanical tabs. National Aeronautics and Space Administration, 1989.
Find full textEd, Nelson, and United States. National Aeronautics and Space Administration., eds. Comparison of 3D computation and experiment for non-axisymmetric nozzles. National Aeronautics and Space Administration, 1989.
Find full textCenter, Ames Research, ed. Supersonic laminar flow control research: Final report, July 1994-June 1996. University of Tennessee, Space Institute, 1996.
Find full textCenter, Ames Research, ed. Supersonic laminar flow control research: Semiannual report #4, July 1995-December 1995. Ames Research Center, 1995.
Find full textG, Wiberg Clark, and United States. National Aeronautics and Space Administration., eds. Supersonic laminar flow control research: NASA grant no. NAG 2-881, final report, January 1994 - June 1996. National Aeronautics and Space Administration, 1996.
Find full textStitt, Leonard E. Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textStitt, Leonard E. Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textGanesh, Raman, and United States. National Aeronautics and Space Administration., eds. Supersonic jets from bevelled rectangular nozzles. National Aeronautics and Space Administration, 1993.
Find full textMcArdle, Jack G. Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft. National Aeronautics and Space Administration, 1992.
Find full textMcArdle, Jack G. Internal reversing flow in a tailpipe offtake configuration for SSTOVL aircraft. National Aeronautics and Space Administration, 1992.
Find full textR, Kadambi J., and United States. National Aeronautics and Space Administration., eds. Generation of monodisperse droplets by spontaneous condensation of flow in nozzles: Final technical report. Dept. of Mechanical and Aeropsace [i.e. Aerospace] Engineering, Case Western University, 1993.
Find full textR, Hingst Warren, and United States. National Aeronautics and Space Administration., eds. Progress toward synergistic hypermixing nozzles. National Aeronautics and Space Administration, 1991.
Find full textSidorov, L. V. (Leonid Vasilʹevich), 1906-1988, ред. Raschet sverkhzvukovykh techeniĭ v piramidalʹnykh soplakh. Vychislitelʹnyĭ ͡tsentr RAN, 1991.
Find full textDavis, D. O. Progress toward synergistic hypermixing nozzles. American Institute of Aeronautics and Astronautics, 1991.
Find full textWolf, Stephen W. D. Supersonic wind tunnel nozzles: A selected, annotated bibliography to aid in the development of quiet wind tunnel technology. National Aeronautics and Space Administration, 1990.
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