Adjustment of Aerodynamic-Compensation Characteristics of a Pitot Tube by Rear-Body Shape Manipulation

Author:

Masud Jehanzeb1,Akram Farooq bin2

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Institute of Avionics and Aeronautics, Air University, Islamabad 44000, Pakistan

2. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332

Abstract

In this paper we present a methodology for adjustment of subsonic compensation characteristics of an aerodynamic-compensation Pitot tube. This methodology is based on manipulation of a Pitot tube profile (shape) downstream of the static pressure port such that its subsonic characteristics are modified while the supersonic characteristics remain unchanged. Due to this “rear-body” shape adjustment, complete redesign of a developed or in service Pitot tube is not required. We have used computational fluid dynamics tools in the analysis and design refinement of a Pitot tube by rear-body shape adjustment. The complete Mach number regime (M<2) has been computationally analyzed for three different rear-body profiles. The results of our study indicate that significant variation in subsonic compensation characteristics of a Pitot tube is possible by this method.

Publisher

ASME International

Subject

Mechanical Engineering

Reference17 articles.

1. Garcy, W. , 1980, “Measurement of Aircraft Speed and Altitude,” NASA Reference Publication No. 1046.

2. Letko, W. , 1947, “Investigation of the Fuselage Interference on a Pitot-Static Tube Extending Forward From the Nose of the Fuselage,” NASA, Report No. NACA-TN-1496.

3. Ritchie, V. S. , 1959, “Several Methods for Aerodynamic Reduction of Static-Pressure Sensing Errors for Aircraft at Subsonic, Near-Sonic, and Low Supersonic Speeds,” NASA, Technical Report No. TR R-18.

4. Computation of Transonic Aerodynamically Compensating Pitot Tube;Luo;J. Aircr.

5. Robust Design of an Aerodynamic Compensation Pitot-Static Tube for Supersonic Aircraft;Latif;J. Aircr.

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