Simple technique for frequency-response enhancement of miniature pressure probes

AIAA journal

Volumn 37, Issue 7, 1999, Pages 897-899

  Rediniotis, Othon K ^a   Pathak, Mahesh M ^a  

^a TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; FREQUENCY RESPONSE; MATHEMATICAL MODELS; MINIATURE INSTRUMENTS; NAVIER STOKES EQUATIONS; PRESSURE DROP; PRESSURE MEASUREMENT; PROBES; REAL TIME SYSTEMS;

PNEUMATIC DISTORTION; PRESSURE PROBES; PROBE TUBING SYSTEM;

PRESSURE TRANSDUCERS;

EID: 0033165474     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7539     Document Type: Article

References (5)

1. Whitmore, S. A., and Leondes, C. T., "Pneumatic Distortion Compensation for Aircraft Surface Pressure Sensing Devices," Journal of Aircraft, Vol. 28, No.12, 1991, pp. 828-836.
2. Huston, W. B., "Accuracy of Airspeed Measurements and Flight Calibration Procedures," NACA Rept. 919, Feb. 1948.
3. Wildhack, W, A., "Pressure Drop in Tubing in Aircraft Instrument Installations," NACA TN-593, Feb. 1937.
4. Whitmore, S. A., and Moes, T. R., "The Effects of Pressure Sensor Acoustics on Airdata Derived from a High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System," NASA TM-101736, Feb. 1991.
5. Pathak, M., "A Simple Technique for Frequency Response Enhancement of Miniature Pressure Probes," M.S. Thesis, Aerospace Engineering Dept., Texas A&M Univ., College Station, TX, Dec. 1998.