Research and development in instrumentation for static testing
Development of instrumentation for static testing
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Development of instrumentation for static testing
Force tests to determine static and dynamic longitudinal stability derivatives of powered scale model of tilt-wing V/STOL transport aircraft
Hypersonic static stability investigation of Tomahawk rocket model
Data acquisition of acoustic, vibration and heat flux during static rocket testing, using balloon rigging arrangement
Text on deformable solid statics including indeterminate systems, strain, stress, elasticity, continuum energy, plasticity and mathematical appendix
Predictability of winds and virtual temperature profiles for flight and static test operations, establishing forecast verification criteria
Response of impact and static pressure probes in rarefied high speed gas flow
Effects of jet pluming on static stability of ballistic bodies at Mach number of 6.00
Literature survey and experiments on stress deformation characteristics of solids under static loading
Flip-flop arrays, power transistors, epitaxial stress, and other technological developments in integrated static inverter program
Low subsonic static and dynamic stability characteristics of blunt 120 deg conical configuration
Static aerodynamic characteristics of model of subsonic jet transport aircraft at Mach numbers from 0.40 to 1.20
Static longitudinal aerodynamic characteristics of decelerator vehicle scale model
Timing channel circuit reliability in static inverter
Static aerodynamic characteristics of aborted Apollo-Saturn V vehicle
Local heat transfer and static pressure data for steam condensation in vertical downflow tube
Component reliability analysis for 250 volt-ampere static inverter
Static stability of sounding rocket at Mach numbers 1.50 to 4.63 to determine effect of body length and fin cant