Stress corrosion of titanium alloys under simulated supersonic flight conditions
Simulated study of effects of high altitude supersonic air flow on titanium alloy hot salt cracking process
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Simulated study of effects of high altitude supersonic air flow on titanium alloy hot salt cracking process
Air flow heat transfer in annular channels with resistance provided by aperture roughness
Hydrodynamics and heat transfer of heated air flowing in tube with turbilizers on heat transfer surface
Helium and air flow tests over single flat plates to determine dynamic pressure limits of nuclear fuel element plates
Vertical laminar air flow and acceleration of die-off rate of heterotrophic mesophilic bacteria and vegetative cells with spores
Spherical piston problem extended to include effects of equilibrium chemistry on air flow
Aerodynamic and thermodynamic calibration of nonequilibrium air flow in Ames 1-foot shock tunnel
Handbook, laminar air flow facility, lunar quarantine information system, and model studies for spacecraft contamination control
Vortex at air intake inlet investigated by direct air flow visualization techniques
Computer analysis of total pressure loss and air flow distribution in annular flow gas turbine combustion chambers
Multiple function combination probe design for compressor and turbine air flow research
Three dimensional laser Doppler instrument measures both local mean and fluctuating gas velocity of air flow. Technique is used for measuring atmospheric wind velocity and turbulence. Under certain conditions liquid flows can be measured.
Determining entrainment of entrapped liquid as function of air flow, and viscosity
Air flow and vacuum effects on damping between solid-solid sliding interfaces in aluminum space structures in relation to surface oxide layers
Wind tunnel air flow modulating device and apparatus for selectively generating wave motion in wind tunnel airstream
Stable operating range of supersonic mixed compression inlet increase by air flow removal via throat bleed system
Turboramjet powered hypersonic aircraft axisymmetric inlet systems using forward translating cowl and centerbody for various air flow characteristics
Radiative cooling of shock heated air in cylindrical shock tubes, calculating enthalpy profiles for nonadiabatic air flow