Formulaton of a general technique for predicting pneumatic attenuation errors in airborne pressure sensing devices
- 18 May 1988
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Response of Pneumatic Transmission Lines to Step InputsJournal of Basic Engineering, 1959
- The Influence of Geometry Parameters Upon Lag Error in Airborne Pressure Measuring SystemsPublished by Defense Technical Information Center (DTIC) ,1957
- Attenuation of oscillatory pressures in instrument linesJournal of Research of the National Bureau of Standards, 1950