1–50 von 71 Ergebnissen
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    A computational method for determining detonation cell size

    KAILASANATH, K. / ORAN, E. / BORIS, J. et al. | AIAA | 1985

    Acoustic-vortex interactions and low frequency oscillations in axisymmetric combustors

    KAILASANATH, K. / GARDNER, J. / BORIS, J. et al. | AIAA | 1987

    Adaptive unstructured mesh methods for steady viscous flow

    HASSAN, O. / MORGAN, K. / PROBERT, E. et al. | AIAA | 1991

    Analysis of transient flows in thermally choked ram accelerators

    LI, CHIPING / KAILASANATH, K. / ORAN, E. et al. | AIAA | 1993

    An overview of results from the ion diagnostics sensors flown on DS1

    Brinza, D. / Henry, M. / Mactutis, A. et al. | AIAA | 2001

    An overview of the microgravity environment and its effects on science

    DeLombard, R. / Nelson, E. / Alexander, J. et al. | AIAA | 1996

    A numerical study of an unsteady diffusion flame

    LASKEY, K. / ELLZEY, J. / ORAN, E. | AIAA | 1989

    Application of skin technology to turbine blades

    WORTMANN, J. / SCHWEITZER, K. / SPRENGER, H. et al. | AIAA | 1978

    Approximate convective heating equations for hypersonic flows

    ZOBY, E. / MOSS, J. / SUTTON, K. | AIAA | 1979

    Artificial Gravity During Bed Rest Deconditioning: A Case Report

    Paloski, William H. / Young, Laurence R. / Arya, Maneesh et al. | AIAA | 2006

    A study of heterogeneous detonations

    RAGLAND, K. / DABORA, E. / NICHOLLS, J. | AIAA | 1966

    Best Practices for Reliable and Robust Spacecraft Structures

    Raju, I / Murthy, Pappu / Patel, N et al. | AIAA | 2007

    Boiling limits in heat pipes with annular gap wick structures

    WOLOSHUN, K. / SENA, J. / KEDDY, E. et al. | AIAA | 1990

    Computational studies of a localized supersonic shear layer

    BORIS, J. / ORAN, E. / GARDNER, J. et al. | AIAA | 1989

    Design and performance evaluation of a two-position variable geometry turbofan combustor

    SANBORN, J. / SCHEIHING, P. / COLEMAN, E. et al. | AIAA | 1984

    Downstream mixing gasdynamic lasers - A numerical solution

    PARTHASARATHY, K. / ANDERSON, JR., J. / JONES, E. | AIAA | 1979

    Effects of energy release on high-speed flows in an axisymmetric combustor

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1989

    Heat pipe avionic thermal control

    TOKEN, K. / GARNER, E. / COOK, R. et al. | AIAA | 1980

    Improvement of disk MHD generator performance by inlet swirl

    Yamasaki, H. / Okuno, Y. / Torii, S. et al. | AIAA | 1999

    Initial radiation measurement results from Europe's Galileo test-bed satellite, Giove-A

    Ryden, K. A. / Morris, P. A. / Rodgers, D. J et al. | AIAA | 2006

    Interactions between acoustics and vortex structures in a central dump combustor

    KAILASANATH, K. / GARDNER, J. / BORIS, J. et al. | AIAA | 1986

    Introducing the ESA DRAMA Tool

    Martin, C. E. / Cheese, J. E. / Sánchez-Ortiz, N. et al. | AIAA | 2004

    IVHM (Integrated Vehicle Health Management) techniques for future space vehicles

    Baroth, E. / Powers, W. / Fox, J. et al. | AIAA | 2001

    Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone

    STETSON, K. / THOMPSON, E. / DONALDSON, J. et al. | AIAA | 1983

    Laser and radiofrequency production of seeded air plasmas

    Scharer, J. / Ding, G. / Gui, H. et al. | AIAA | 1999

    Line relaxation methods for the solution of 2D and 3D compressible flows

    HASSAN, O. / PROBERT, E. / MORGAN, K. et al. | AIAA | 1993

    Mars Exploration Deep Space Return Link Scenarios ...

    Noreen, Gary K. / Williams, W. Dan / Sands, O. Scott et al. | AIAA | 2005

    Measurement of dynamic cross-derivatives due to pitching and yawing

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1974

    Monolithic Fuel Cells

    Fee, D. C. / Billone, M. C. / Busch, D. E. et al. | AIAA | 1987

    New concept of small satellite, HETE-2 and its sci...

    Matsuoka, M. / Kawai, N. / Yoshida, A. et al. | AIAA | 2005

    Numerical simulations of flow modification of supersonic rectangular jets

    Kolbe, R / Kailasanath, K / Young, T et al. | AIAA | 1995

    Numerical simulations of high-speed flows in an axisymmetric ramjet

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1988

    Numerical simulations of the reactive flow field in an axisymmetric combustor

    KAILASANATH, K. / GARDNER, J. / ORAN, E. et al. | AIAA | 1987

    Numerical simulations of transient flows in ram accelerators

    LI, CHIPING / KAILASANATH, K. / ORAN, E. et al. | AIAA | 1993

    Oblique detonation wave studies in the Caltech T-5 Shock Tunnel Facility

    Sterling, J. / Cummings, E. / Ghorbanian, K. et al. | AIAA | 1998

    Optically pumped and controlled electric discharges

    Macheret, Sergey / Barker, P. / Miles, Richard et al. | AIAA | 1999

    Optical measurements of the orbital debris environment

    Jarvis, K. / Africano, J. / Stansbery, E. | AIAA | 2000

    Orbital parameters for objects observed by the Mic...

    Abercromby, K. J. / Seitzer, P. / Parr-Thumm, T. L. et al. | AIAA | 2005

    Passive control of flow separation over delta wings at high angle-of-attack

    Van Dyken, R. / Yu, K. / Gutmark, E. et al. | AIAA | 1996

    Performance of a Low Density Ablative Heat Shield Material

    Covington, M. A. / Balboni, J. A. / Chen, Y-K et al. | AIAA | 2004