Some Performance Characteristics of the LRC 3 3/4-inch Pilot Expansion Tube Using an Unheated Hydrogen Driver
Performance characteristics of expansion tube using room temperature hydrogen driver
FLOW VELOCITY↗
SEARCH · Search NASA
Results for “SHOCK TUNNEL”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Contract-surface tailoring in real shock tubes
Equilibrium pressure measured after interaction of reflected shock with contact surface to determine tailored conditions in real shock tubes
PRESSURE MEASUREMENT↗
Analysis of tailored-interface operation of shock tubes with helium-driven planetary gases
Analysis of tailored interface operation of shock tubes with helium driven planetary gases
REAL GAS↗
Shock-tube investigation of bromine dissociation rates in presence of argon, neon, and krypton
Shock-tube investigation of bromine dissociation rates in presence of argon, neon, and krypton
DISSOCIATION↗
Radiation measurement techniques
Quantitative radiation measurement techniques for electric arc driven hypervelocity shock tube
SHOCK TUNNEL↗
The Calculation of Chemical and Ionization Equilibrium in a Conventional Shock Tube Scientific Report No. 12
Calculating chemical and ionization equilibrium of plasma in conventional shock tube
THERMODYNAMIC EQUILIBRIUM↗
Experimental assessment of the effect of large amounts of argon in a planetary atmosphere on stagnation-point convective heating.
Atmospheric argon effect on hypersonic stagnation point convective heat transfer, using arc-heated shock tube simulating flight velocities up to 34,000 fps
ARGON↗
Study of equilibrium air total radiation.
Equilibrium air total radiation mechanism, vacuum UV radiation and relation to hypervelocity entry studied, using shock tube blunt model test flow
ATMOSPHERIC RADIATION↗
Some performance characteristics of the LRC 3-3/4-INCH pilot expansion tube using an unheated hydrogen driver.
Flow velocity, static pressure and test-section pitot pressure of expansion tube, using unheated /room temperature/ hydrogen driver
FLOW VELOCITY↗
Evaluation of flow properties in a combustion- driven expansion tube operating at 7.5 km/sec.
Convective and radiative heat transfer during atmospheric reentry examined, using double- diaphragm shock tube operated in expansion tube mode
RADIATIVE HEAT TRANSFER↗
Analytical and experimental investigation of internal resistance shock tube driver gas heating systems.
Internal resistance shock tube driver gas heating system to heat helium driver gas to 1000 degrees F at 15,000 psia
SHOCK TUNNEL↗
Explosive compression and acceleration of helium for hypervelocity applications.
Glass tube containing pressurized helium progressively imploded by coaxial explosive charge, considering application to hypervelocity guns
HELIUM↗
Association of CN in an expansion wave.
Kinetics of CN radicals association generated by shocking cyanogen-argon mixtures at high temperatures in reflected shock region of expansion wave
GAS MIXTURE↗
Line-reversal measurements of excitation and electron temperature in a shock tube.
Population temperatures within argon-calcium plasma generated by reflected aerodynamic shock determined by spectral line-reversal method
SHOCK TUNNEL↗
Recombination of carbon monoxide and atomic oxygen at high temperatures.
Recombination of carbon monoxide and atomic oxygen in expansion wave at high temperature in single pulse shock tube
OXYGEN RECOMBINATION↗
Isotope exchange rates. III - The homogeneous four-center reaction H sub 2 plus D sub 2.
Homogeneous isotopic exchange reaction between hydrogen and deuterium in single-pulse shock tube with excess argon
CHEMICAL REACTION↗
Fast-response total thermal radiation detectors.
Thin film thermal radiation detector noting construction, calibration, performance, error sources and advantages of pyroelectric over thin film gauges
RADIANT ENERGY↗
Vacuum ultraviolet sensitive total radiation gage system.
Windowless total radiation gauge for shock tube measurements of high temperature gas radiance
SHOCK TUNNEL↗