Heart rate response to sound and light.
Human heart rate response to different intensities of sound and light
SEARCH · Engineering Papers
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.
Human heart rate response to different intensities of sound and light
Physical and temporal aspects of sound which influence the rating of subjective noisiness are intensity, spectrum shape and bandwidth, spectral complexity, and duration. Objective rating methods include a graphic method, full octave and one-third octave methods, and methods that measure one value over all frequencies.
Wall design effects of air intake duct in axial compressor on sound propagation
Surface roughness effects of bar on vortex sound and aerodynamic drag generation during move through air
Sound propagation in cylindrical pipe with streamlined impedance walls
Development of vibration test levels for sounding rocket subassemblies
Combined range rate and telemetric interferometer system for radar tracking of scientific sounding rockets
Data evaluation for upper atmosphere falling sphere soundings
Computer program for determining third octave sound spectra in acoustic test data
Sound measurements on 4000 pound thrust high bypass ratio turbofan engine
Refraction of sound by temperature and velocity profiles in jet flow
Analysis of current meteorological rocket sounding systems for 30 km to 200 km region
Literature review on meteorological rockets and system requirements and techniques for upper atmosphere sounding
Cochlear hair-cell loss in guinea pigs after intense sinusoidal sound stimulation
Sound absorption in acoustically treated ducts in presence of oblique waves
Instruction procedures for training military personnel to install and operate omnidirectional sound locating set
Theoretical and experimental model study of sound induced vibration transmitted to shroud enclosed spacecraft
Graphical method for determining sounding rocket attitudes from optical sensor and flux gate magnetometer data