1–20 von 71 Ergebnissen
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    Accuracy of modal stress calculations by the finite element method

    ADELMAN, H. M. / CATHERINES, D. S. / WALTON, W. C. | AIAA | 1970

    A computer system for aircraft flyover acoustic data acquisition andanalysis

    BOSTON, D. W. / CASHAR, E. E. / COPE, D. A. et al. | AIAA | 1984

    A Cooled Laminated Radial Turbine Technology Demonstration

    Roy W. Vershure Gerold D. Large / Leonard J. Meyer / Jan M. Lane | AIAA | 1981

    Aeroassist flight experiment heating-rate sensitivity study

    ROCHELLE, W. C. / TING, P. C. / BOUSLOG, S. A. et al. | AIAA | 1991

    Aerodynamic Characteristics of an Unsteady Separated Flow

    M. S. Francis / J. E. Keesee / J. D. Lang et al. | AIAA | 1979

    Alleviation of the subsonic pitch-up of delta wings

    RAO, D. M. / JOHNSON, T. D. | AIAA | 1983

    Analysis of engine usage data for tactical systems

    MAY, R. J. / CHAFFEE, D. R. / STUMBO, P. B. et al. | AIAA | 1983

    Analysis of multifastener composite joints

    Griffin, O. H. / Hyer, M. W. / Cohen, D. et al. | AIAA | 1994

    A realistic interstellar explorer

    McNutt, R.L Jr. / Andrews, G.B / Gold, R.E et al. | Elsevier | 2003

    Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20

    FISCHER, M. C. / MADDALON, D. V. / WAGNER, R. D. | AIAA | 1971

    Comparisons of boundary-layer transition measurement techniques at supersonic Mach numbers

    HALL, R. M. / CARRAWAY, D. L. / JOHNSON, C. B. et al. | AIAA | 1991

    Control of hypersonic aerodynamic forces with surface blowing

    MESSITER, A. F. / ADAMSON, T. C. / MATARRESE, M. D. | AIAA | 1991

    Design data for a disk rotating in a rarefied environment

    BARBEE, D. G. / NEWELL, P. H. | AIAA | 1971

    Design of a Dual Wide-Angle Visual Cue Simulator

    J. L. COPELAND / W. M. KAHLBAUM L. E. BARKER G. G. STEINMETZ AND R. D. GROVES | AIAA | 1971

    Destination pluto: New horizons performance during the approach phase

    Flanigan, Sarah H. / Rogers, Gabe D. / Guo, Yanping et al. | Elsevier | 2016

    Determination of tire-wheel interface loads for aircraft wheels

    Kandarpa, S. / Spencer, B. F. / Kirkner, D. J. et al. | AIAA | 1994

    Development of an Aeroballistic Range Capability for Testing Re-Entry Materials

    G. D. Norfleet / R. E. Hendrix / R. M. Raper et al. | AIAA | 1975

    Development of Theoretical Models for Jet-Induced Effects on V/STOL Aircraft

    M. J. Siclari / D. Migdal / T. W. Luzzi J. Barche et al. | AIAA | 1976