Analysis Method for the Design of Compensated Pitot-Static Probes for Use on General Aviation Aircraft Mississippi State Univ

Format:

Conference/Event

Author/Creator:

Daiber, Mark P., author.

Conference Name:

Aerospace Atlantic Conference & Exposition (1995-05-23 : Dayton, Ohio, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1995

Summary:

Pitot-static probes are used on aircraft to measure total and static pressure, necessary for airspeed and altitude information. Aerodynamic compensation is often desired to obtain accurate freestream static pressure readings when the instrument is located near regions of disturbed flow generated by the aircraft's forebody. In this study, computational fluid dynamics (CFD) has been used to analyze surface pressures on the forebody, the probe, and on forebody/probe configurations for a transonic business jet. Compensation techniques and validation cases are presented. Results indicate that CFD can be effective in locating static pressure ports in a region of zero pressure coefficients (Cp)

Notes:

Vendor supplied data

Publisher Number:

951431

Access Restriction:

Restricted for use by site license