Tilt table and plasma volume changes with short term deconditioning experiments.
Tilt table response and plasma volume changes in experimental subjects evaluated before and after short term periods of deconditioning
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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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The use of tilt table studies to evaluate cardiovascular deconditioning of space flight
Use of tilt table studies to evaluate cardiovascular deconditioning of space flight
Vogt, F. B.↗
Effect of ground proximity on the longitudinal, lateral, and control aerodynamic characteristics of a tilt-wing four-propeller V/STOL model
Ground proximity effects on longitudinal, lateral, and control aerodynamic characteristics of tilt wing four propeller V/STOL wind tunnel model
Goodson, K. W.↗
Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests
Aerodynamic factors, and effects on dynamic longitudinal stability characteristics of tilt wing V/STOL aircraft
Chambers, J. R.↗
Design of a precision tilt and vibration isolation system
Precision tilt and vibration isolation system design
Weinstock, H.↗
Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane
Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft
Deckert, W. H.↗
Tilt and vibration isolation system Final evaluation report
Design feasibility of precision tilt and angular vibration isolation system using gyroscope and accelerometer instruments for control
Rhodes, B.↗
Discussion of paper by R.W. Fredricks, E. W. Greenstadt, and C. P. Sonett, ''Magnetodynamically induced ambiguity in the data from tilted, spinning fluxgate magnetometers- Possible application to IMP 1.''
Critical review of argument by Fredericks et al concerning ambiguity of IMP 1 data obtained from tilted spinning fluxgate magnetometers
Ness, N. F.↗
Material considerations for high temperature tilting pad gas bearings.
Sliding contact problems in tilting pad gas bearings at high temperatures, considering material selection
Murray, S. F.↗
Design of a precision tilt and rotational vibration isolation system for inertial sensor testing.
Precision tilt and rotational isolation system design for inertial navigation sensor testing
Weinstock, H.↗
Egocentric localization of the visual horizontal in normal and labyrinthine- defective observers as a function of head and body tilt.
Egocentric localization of visual horizontal in normal and labyrinthine defective observers for various head and body tilts
Clark, B.↗
Apollo spacecraft systems analysis program. Range coverage for the CSM rendezous radar transponder. Antenna raised 4 in. and tilted forward 15 deg
Range coverage diagrams for CSM rendezvous radar transponder antenna raised 4 in. and tilted forward 15 deg
Doty, M. G.↗
Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing
Aerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for modes of propeller rotation
Fink, M. P.↗
Analysis and performance of the gas-lubricated tilting pad thrust bearing Interim report
Optimal design and performance criteria for gas lubricated tilting pad thrust bearing
Colsher, R.↗
Pressure Distribution of a Large Semispan Tilting Wing with 0.4-diameter-chord, Single- Slotted Flap, and a Single Propeller 0.22 Chord Below Wing
Aerodynamic pressure distribution on semispan tilting wing-propeller combination of V/STOL aircraft
Fink, M. P.↗
Cardiovascular changes during tilt and leg negative pressure tests.
Cardiovascular changes in male students during tilt and negative pressure tests with bed rest studied from heart rate, blood pressure and leg volume measurements
Bartok, S. J.↗
Analysis and performance of the gas-lubricated tilting pad thrust bearing.
Gas lubricated tilting pad thrust bearing analysis and performance, determining optimum hydrodynamic crown profile
Colsher, R.↗
Relative energies of /1100/ tilt boundaries in aluminum oxide.
Aluminum oxide relative grain boundary energy and surface diffusion coefficient, considering thermal grooving of bicrystals with symmetrical tilt boundaries
Scott, W. D.↗