Suggested test of a self-calibrating baro- height reporting concept for general aviation and airline SSR Interim scientific report
Self-calibrating baro-altitude concept for general aviation
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Self-calibrating baro-altitude concept for general aviation
Navigation-aids identification decoder and display device for general aviation aircraft
NASA civil aviation electronics research program, discussing feasibility of V/STOL aircraft all-weather operations
General aviation missions in national transportation system /1968, 1975, 1980/, considering fuel taxes, overall system economics, ground facilities, etc
Annual general aviation aircraft accident rate variation related to annual variations in pilot flight training activity
Civil aviation research and development for flight vehicles
Civil aviation growth assessment requiring Federal Government research and development in airports, noise, and air traffic control
General aviation weather avoidance sensor study
Workload relieving displays and controls for general aviation, discussing feasibility of digital computer driven integrated displays
Antenna design for single engine light general aviation aircraft weather radar, reviewing attenuation and terrain return problems
Cost reduction procedures for aircraft turbine engines used in civil aviation
Investigation of angle of attack information display for pilots to increase efficiency of general aviation aircraft operation
Benefits and problems of using head-up displays in commercial and general aviation aircraft
Review of policies affecting civil aviation, problems confronting it, and potential for future contributions to national benefits
Civil aviation research and development projects noting characteristics and growth to date, current problems, future requirements, potential solutions, and recommendations
An analysis is presented of 79 000 hours of data obtained from NASA V -G and VGH flight recorders installed on 134 general aviation aircraft engaged in eight types of operations. Information is presented on typical mission characteristics, on airspeed practices, on gust accelerations and derived gust velocities encountered, on maneuver -acceleration experience, and on the initial positive landing-impact accelerations. Comparisons are also made of the actual gust and maneuver loads experienced with the design gust and maneuver loads.
Sensitivity analysis of advance propeller configurations designed for general aviation aircraft of 1980 time period
Potential impact of advanced technology in 1985 on four types of general aviation aircraft including STOL V/STOL, and helicopters