The Dryden Flight Loads Research Facility (NASA) and the associated equipment for simulating the loading and heating of aircraft or their components are described. Particular emphasis is placed on various fail-safe devices which are built into the equipment to minimize the possibility of damage to flight vehicles. The equipment described includes the ground vibration and moment of inertia equipment, the data acquisition system, and the instrumentation available in the facility for measuring load, position, strain, temperature, and acceleration
Device facilitates pilot control of g-load maneuvers and provides immediate indication of g-load con...
The 8 ft. by 15 ft. thermal vacuum chamber (TVAC), housed in Building 1250 at the NASA Langley Resea...
Around 1970, the Y-F-12A loads and structures efforts focused on numerous technological issues that ...
The National Aero-Space Plane (NASP) has renewed interest in hypersonic flight and hot-structures te...
The Integrated Test Facility, built at the NASA Dryden Flight Research Facility, provides new real-t...
The Dryden Flight Research Facility has developed a unique research facility for conducting aerodyna...
NASA Dryden Flight Research Center (DFRC) is working with the United States Navy to complete ground ...
The testing conducted on LaRC-developed hardware for the controlled impact demonstration transport a...
A tire and landing gear test facility has been developed and incorporated into a Convair 990 aircraf...
Instrumentation and drop testing techniques for investigating flight vehicle and personnel protectiv...
An inventory of test facilities for conducting acceleration, environmental, impact, structural shock...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
The Dryden Flight Research Facility has been a leader in developing simulation as an integral part o...
Electrical, mechanical, and operational aspects of a test cell assembly for studying rotating fluids...
The road load simulator facility located at the NASA Lewis Research Center enables a propulsion syst...
Device facilitates pilot control of g-load maneuvers and provides immediate indication of g-load con...
The 8 ft. by 15 ft. thermal vacuum chamber (TVAC), housed in Building 1250 at the NASA Langley Resea...
Around 1970, the Y-F-12A loads and structures efforts focused on numerous technological issues that ...
The National Aero-Space Plane (NASP) has renewed interest in hypersonic flight and hot-structures te...
The Integrated Test Facility, built at the NASA Dryden Flight Research Facility, provides new real-t...
The Dryden Flight Research Facility has developed a unique research facility for conducting aerodyna...
NASA Dryden Flight Research Center (DFRC) is working with the United States Navy to complete ground ...
The testing conducted on LaRC-developed hardware for the controlled impact demonstration transport a...
A tire and landing gear test facility has been developed and incorporated into a Convair 990 aircraf...
Instrumentation and drop testing techniques for investigating flight vehicle and personnel protectiv...
An inventory of test facilities for conducting acceleration, environmental, impact, structural shock...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
The Dryden Flight Research Facility has been a leader in developing simulation as an integral part o...
Electrical, mechanical, and operational aspects of a test cell assembly for studying rotating fluids...
The road load simulator facility located at the NASA Lewis Research Center enables a propulsion syst...
Device facilitates pilot control of g-load maneuvers and provides immediate indication of g-load con...
The 8 ft. by 15 ft. thermal vacuum chamber (TVAC), housed in Building 1250 at the NASA Langley Resea...
Around 1970, the Y-F-12A loads and structures efforts focused on numerous technological issues that ...