Gaseous-helium requirements for the discharge of liquid hydrogen from a 1.52-meter /5-ft/ diameter spherical tank
Gaseous-helium requirements for discharge of liquid hydrogen from 5-ft diameter spherical tank
De Witt, R. L.↗
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Absolute strain measurements with a 30 meter vacuum interferometer
Vacuum interferometer strain gage for absolute earth strain measurement via length change comparison with wavelength standard
Barger, R. L.↗
Gaseous-helium requirements for the discharge of liquid hydrogen from a 3,96-meter-/13 ft/ diameter spherical tank
Helium gas requirements for liquid hydrogen expulsion from spherical tank
De Witt, R. L.↗
Extreme distributions of ground winds /3 to 150 meters/ at Cape Kennedy, Florida
Statistical analysis of wind distribution probabilities at Cape Kennedy
Johnson, B. C.↗
Real gas effects in flow metering
Real gas corrections to gas flow computations for sonic nozzles
Johnson, R. C.↗
Low-speed jet noise from a 1.83 meter /6ft/ fan for turbofan engines
Determination of low speed jet noise from fan engine for simulated nacelle configuration
Feiler, C. E.↗
Automatic signal range selector for metering devices Patent
Voltage range selection apparatus for sensing and applying voltages to electronic instruments without loading signal source
Camp, E. L.↗
Propellent mass distribution metering apparatus Patent
Electronic recording system for spatial mass distribution of liquid rocket propellant droplets or vapors ejected from high velocity nozzles
Ayvazian, R. A.↗
Gas low pressure low flow rate metering system Patent
Flowmeters for sensing low fluid flow rate and pressure for application to respiration rate studies
Fagot, R. J.↗
Two primary methods of proving gas flow meters
Methods for determining mass flow rates of gases for use in calibrating gas flowmeters
Arnberg, B. T.↗
Calibration of Low H2O meter
Low hygrometer calibration for water vapor measurements smaller than 3 mm
Cruikshank, D. P.↗
Real-gas effects in flow metering
Real gas mass flow rate computation through sonic nozzle
Johnson, R. C.↗
Low-speed jet noise from a 1.83-meter /6-ft/ fan for turbofan engines
Fan induced low speed jet noise from turbofan engines, discussing results of far field sound measurements for simulated nacelle configurations with and without acoustic liners
Feiler, C. E.↗
Pressure sensitive gas flow meter
Regulator, which increases flow area in discrete steps as upstream pressure falls, maintains steady flow rate of gas as the supply pressure from storage system decreases.
Hallum, C. E.↗
Metered oxygen supply aids treatment of domestic sewage
Microbiological fixed-bed process was developed in which supplementary oxygen required by microbial species is supplied by electrochemical device. Rate of addition of oxygen to waste treatment process is controlled to maintain aerobic metabolism and prevent anaerobic metabolisms which produce odorous or toxic products.
Weliky, N.↗
An optical quality meter suitable for cryogenic liquids
Construction of instrument to measure ratio of liquid to gas of flowing transparent cryogenic fluid is described. Instrument consists of collimated light source and photoconductive cell. Operation of instrument is described and illustration of equipment is provided.
Hobart, H. F.↗
Combustion products generating and metering device
An apparatus for generating combustion products at a predetermined fixed rate, mixing the combustion products with air to achieve a given concentration, and distributing the resultant mixture to an area or device to be tested is described. The apparatus is comprised of blowers, a holder for the combustion product generating materials (which burn at a predictable and controlled rate), a mixing plenum chamber, and a means for distributing the air combustion product mixture.
Wiberg, R. E.↗
Deployment loads data from a free-flight investigation of all flexible parawings having 371.612 sq meters (4000 sq feet) of wing area
A free-flight test program to determine the deployment characteristics of all-flexible parawings was conducted. Both single-keel and twin-keel parawings having a wing area of 4000 square feet with a five-stage reefing system were tested by use of a bomb-type instrumented test vehicle. Several twin-keel-parawing tests were also made by using an instrumented controllable sled-type test vehicle. The systems were launched from either a C-130 or a C-119 carrier airplane, and a programer parachute was used to bring the test vehicle to a proper dynamic pressure and near-vertical flight path prior to deployment of the parawing system. The free-flight deployment loads data are presented in the form of time histories of individual suspension-line loads and total loads.
Croom, D. R.↗