Performance in air of 4 inch /10.16-cm/ mean-diameter single stage axial-flow turbine for Reynolds numbers from 4,900 to 188,000
Reynolds number effect on single stage axial flow turbine in air
Klassen, H. A.↗
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Results for “000”
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.
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Proton and helium nuclei cosmic ray spectra and modulations between 100 and 2,000 MeV/nucleon
Combination Cerenkov and scintillation detector, and range scintillator for proton and helium nuclei cosmic ray spectra between 100 and 2000 MeV/nucleon
Ormes, J. F.↗
Peculiarities of Mach reflection of shock waves moving in carbon dioxide and nitrogen at velocities on the order of 2,000 m/sec
Peculiarities of Mach reflection of shock waves moving in carbon dioxide and nitrogen at supersonic speeds
Gvozdeva, L. G.↗
Method of Determination of Ion Temperature by the Variations of Satellite Induced Ion Trap Currents and Estimate of the Upper Limit of Ion Temperature at Altitudes of 10,000 Kilometers and Higher According to Data of AES Electron-2
Ion temperature determination by variations of satellite induced ion trap currents - Electron 2 satellite measurements of ion temperatures in ionosphere
Bezrukikh, V. V.↗
FM handling and analog-to-digital conversion of biomedical data from a 1,000-flight study
FM data handling facility for preparing analog physiological data obtained in flight for digital computations
Carpenter, R.↗
Recording and signal-conditioning techniques and equipment used in a 1,000-flight biomedical study
Signal conditioning methods and equipment used for inflight recording of pilot biomedical data
Carpenter, R.↗
Stabilizing effects of several injector face baffle configurations on screech in a 20,000 pound-thrust hydrogen-oxygen rocket
Stability effects of several injector face baffle configurations on screech in hydrogen-oxygen rocket
Bloomer, H. E.↗
Creep of tantalum T-222 alloy in ultrahigh vacuum for times up to 10,000 hours
Creep behavior of tantalum alloys in ultrahigh vacuum for extended time periods
Titran, R. H.↗
Tables of Fe I line intensities. Volume 1 - Temperatures from 1000 deg to 6500 deg K. Volume 2 - Temperatures between 6500 deg and 20,000 deg K
Atomic line intensity tables for ionized iron atom at high temperatures
Borucki, W. J.↗
The solar constant and the solar spectrum measured from a research aircraft at 38,000 feet
Solar constant and spectrum measured from Convair 990 aircraft at 38000 feet
Source record↗
Sonic boom ground pressure measurements for flights at altitudes in excess of 70,000 feet and at Mach numbers up to 3.0
Sonic boom ground pressure measurements for SR-71
Maglieri, D. J.↗
Total radiation measurements at the stagnation point of blunt bodies at stagnation temperatures to 15,000 deg K.
Blunt bodies stagnation point radiation intensity measurements in supersonic flow at very high stagnation temperatures generated by constricted arc heaters
Winovich, W.↗
Experiments on the pressure drop created by a sphere settling in a viscous liquid. II - Reynolds numbers from 0.2 to 21,000.
Pressure drop measurements created by spherical particle settling in viscous fluid for wide Reynolds number range
Brenner, H.↗
Simultaneous observations of a pulsating radio source over a 5,000 km baseline.
Pulsar CP 1919 observed simultaneously at Arecibo and Stanford, discussing interstellar scintillation as possible explanation for amplitude variations
Comella, J. M.↗
Solar spectral irradiance measured from 38,000 feet with a Leiss monochromator and a photoelectric filter radiometer.
Solar spectral irradiance measured by airborne instruments, discussing construction, calibration, etc, of photoelectric filter radiometer and Leiss monochromator
Webb, J. J.↗
Planetary entry body heating rate measurements in air and Venus atmospheric gas up to T equal 15,000 deg K.
Convective plus radiative shock tube model stagnation point heating rate measurements for planetary entry heating rate in air and Venus gas
Livingston, F.↗
A 500,000 sample per second digital recorder for the Ames electric arc shock tunnel.
Digital data acquisition system with ultrahigh sampling rate for Ames electric arc shock tunnel, describing analog to digital conversion, data storage, system performance, etc
Mazer, L.↗
Electrostatic Probe Measurements of Plasma Surrounding Three 25,000 Foot Per Second Reentry Flight Experiments
A high-altitude electrostatic probe experiment is described and data are presented for three RAM C reentries at velocities of approximately 25 OOO feet per second. The electron density profiles inferred from the probe measurements are compared with theoretical calculations, and the probable cause of significant disagreement is briefly discussed. Probe measurements during material-addition sequences for radio-blackout alleviation are presented, and comparisons of probe measurements with other pertinent diagnostic measurements are made.
W Linwood Jones, Jr↗