1–50 von 396 Ergebnissen
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    Aerodynamic Model for Tandem Flapping Wings

    Faisal, A. H. M. / Filippone, A. | AIAA | 2016

    Aerodynamic Model for Insect Flapping Wings with Induced Flow Effect

    Faisal, A. H. M. / Filippone, A. | AIAA | 2016

    Issues with Proportional Damping

    Kabe, A. M. / Sako, B. H. | AIAA | 2016

    Pressure Characteristics of an Aerospike Nozzle in a Rotating Detonation Engine

    Schwer, Douglas A. / Brophy, Christopher M. / Kelso, Robert H. | AIAA | 2018

    Heat Transfer Phenomena in a Vortex Engine

    Kargar, M. / Saidi, M. H. / Ghafourian, A. | AIAA | 2009

    Comment on "Cooling Fin Design"

    Soliman, H. M. / Elazhary, A. M. | AIAA | 2008

    Acid Gas Composition Effects on the Optimum Temperature in Claus Reactor

    Selim, H. / Gupta, A. K. / Sassi, M. | AIAA | 2008

    Loss of Control Detection for Commercial Transport Aircraft Using Conditional Variational Autoencoders

    Campbell, Newton H. / Grauer, Jared A. / Gregory, Irene M. | AIAA | 2021

    Film thickness measurements in a simplex swirl atomizer

    LEFEBVRE, A. H. / SUYARI, M. | AIAA | 1986

    OPTIMUM POLAR SATELLITE NETWORKS FOR CONTINUOUS EARTH COVERAGE

    SCHOEN, A. H. / ULLOCK, M. H. | AIAA | 1963

    Assessing Wall-Modeled Large-Eddy Simulation for Low-Speed Flows with Heat Transfer

    Xu, Haosen H. A. / Yang, Xiang I. A. / Milani, Pedro M. | AIAA | 2021

    Effectiveness of Complex Design Through an Evolutionary Approach

    Pedro, H. / Kobayashi, M. H. / Coimbra, C. F. M. et al. | AIAA | 2008

    Aeroelastic Stability of Hingeless Rotor Blades in Hover Using Fully Intrinsic Equations

    Amoozgar, M. R. / Shahverdi, H. / Nobari, A. S. | AIAA | 2017

    Spray Characterization of a Slinger Injector Using a High-Speed Imaging Technique

    Rezayat, S. / Farshchi, M. / Karimi, H. et al. | AIAA | 2017

    Temperature Distribution on a Gas Turbine Shaft Exposed to Swirl Combustor Flue

    Aghakashi, V. / Saidi, M. H. / Mozafari, A. A. et al. | AIAA | 2015

    Flows Generated by Electrohydrodynamic Gas Pumps with Different Electrode Orientations

    Mazumder, A. K. M. Monayem H. / Lai, Feng C. | AIAA | 2023

    Transport Coefficients for High-Temperature Nonequilibrium Air Flows

    M. Fertig / A. Dohr / H.-H. Fr-uacute et al. | AIAA | 2001

    Transport coefficients for high temperature nonequilibrium air flows

    Fertig, M. / Dohr, A. / Fruehauf, H.-H. | AIAA | 1998

    Comparative Study of Biodiesel and Diesel Jets in Gaseous Crossflow

    Farvardin, E. / Johnson, M. / Alaee, H. et al. | AIAA | 2013

    Atmospheric Plasma Thruster: Theory and Concept

    Greig, A. / Birzer, C. H. / Arjomandi, M. | AIAA | 2012

    Numerical Simulation of Plunging Wing Section at High Angles of Attack

    Gross, A. / Agate, M. / Little, J. et al. | AIAA | 2018

    Propulsion research for rocket SSTOS at NAL/KRC

    Kumakawa, A. / Tamura, H. / Niino, M. et al. | AIAA | 1999

    RAMA Experiments Anomalous Thrusts Consistent with a Brans-Dicke Gravitation Model

    Brito, Hector H. / Brito, Claude M. / Brito, Marcos A. | AIAA | 2020

    NASA's Learn-to-Fly Project Overview

    Heim, Eugene H. / Viken, Erik / Brandon, Jay M. et al. | AIAA | 2018

    Enhancement of Forced Convection Using a Two-Stage Electrohydrodynamic Gas Pump

    Mazumder, A. K. M. Monayem H. / Lai, Feng C. | AIAA | 2018

    Buckling of Sandwich Plates with Random Material Properties Using Improved Plate Model

    Pandit, M. K. / Singh, B. N. / Sheikh, A. H. | AIAA | 2009

    Mist cooling ratios analysis in rectangular passage with 45-deg angled rib

    Alhajeri, Hamad M. / Amaral Teixeira, Joao / Addali A., Abdulmajid et al. | AIAA | 2016

    Jet Impingement Heat Transfer Enhancement on a rib-roughened Flat Plate

    Alenezi, A H. / Amaral Teixeira, Joao / Addali A., Abdulmajid et al. | AIAA | 2016

    Particle Toughened Interfaces Enhance Mechanical Response of Composites

    Nguyen, Minh H. / Vijayachandran, Avinkrishnan A. / Davidson, Paul et al. | AIAA | 2019

    Eigenstructure of the State Matrix of Balanced Realizations

    A. M. A. Hamdan / A. H. Nayfeh | AIAA | 1989

    Restart transients of hybrid rocket engines.

    SARANIERO, M. A. / CAVENY, L. H. / SUMMERFIELD, M. | AIAA | 1973

    On the Flow Measurements of Simulated Helicopter Exhausts

    Teo, Z W / Wong, W. H. / Mohamed, M. A. et al. | AIAA | 2020

    Lee-side vortices on delta wings at hypersonic speeds.

    RAO, D. M. / WHITEHEAD, A. H. | AIAA | 1972

    Surface pressure measurements on a body subject to vortex wake interaction

    BRAND, A. G. / MCMAHON, H. M. / KOMERATH, N. M. | AIAA | 1989

    Statistical Combination of Time-Varying Loads

    Sako, B. H. / Kabe, A. M. / Lee, S. S. | AIAA | 2009

    Nonsteady burning phenomena of solid propellants - Theory and experiments.

    KRIER, H. / SIRIGNANO, W. A. / SUMMERFIELD, M. | AIAA | 1968

    Skeletal Mechanism of the Methane Oxidation for Space Propulsion Applications

    Slavinskaya, Nadja / Abbasi, M. / Starcke, J.-H et al. | AIAA | 2016

    Saturating and time-optimal feedback controls

    BIKDASH, M. / CLIFF, E. M. / NAYFEH, A. H. | AIAA | 1993

    AeroMEMS Surface Fence for Wall Shear Stress Measurements in Turbulent Flows

    Schiffer, M. / Obermeier, E. / Grewe, F. et al. | AIAA | 2006

    Soot Surface Growth in Laminar Hydrocarbon/Air Diffusion Flames

    A. M. El-Leathy / C. H. Kim / G. M. Faeth | AIAA | 2003