Numerical Prediction of Two-Phase Reacting Flow Field and Performance in an Aeroengine Combustor
Functional Comparison of Lunar Regoliths and Their Simulants
Power and Propulsion at NASA Glenn Research Center: Historic Perspective of Major Accomplishments
Propulsion and power have long been core competencies of the National Aeronautics and Space Administration (NASA
...Instrumentation for Aerospace Applications: Electronic-Based Technologies
Throughout the 70-year history of the National Aeronautics and Space Administration (NASA) Glenn Research Center
...Nuclear Thermal Propulsion: Past Accomplishments, Present Efforts, and a Look Ahead
In this paper, the steady two-dimensional boundary layer flow of chemical reaction magnetohydrodynamics (MHD
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The exploration and development of space will require energy that is reliable, ubiquitous, and economical to
...Dynamic Simulation of Insulation Material Ablation Process in Solid Propellant Rocket Motor
An analytical study is presented for the effects of chemical reaction and mass transfer on the free convective
...Three-Dimensional Flow of Maxwell Fluid with Soret and Dufour Effects
Prediction of Chemical Nonequilibrium Flow Structure at Different Free-Stream Knudsen Numbers
Design Methodology for the Performance, Weight, and Economic Assessment of Chemical Rocket Engines
The main emphasis of the present study is to discuss the effect of chemical reaction on flow, heat, and mass
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This article explores the steady mixed convection stagnation-point flow of Powell-Eyring fluid in the presence of
...Characteristics of IPN Adhesive Bonding of Polyether Imide to Titanium for Aerospace Application
Development and Geotechnical Engineering Properties of KLS-1 Lunar Simulant