Analysis of an Artificial Tailplane Icing Flight Test of a High-Wing, Twin-Engine Aircraft

Author

Shehzad Maksudahmad Shaikh

Graduation Semester and Year

2016

Language

English

Document Type

Thesis

Degree Name

Master of Science in Aerospace Engineering

Department

Mechanical and Aerospace Engineering

First Advisor

Baxter R Mullins

Abstract

The US Air Force Flight Test Center (AFFTC) conducted a civilian, Federal Aviation Administration (FAA) sponsored, evaluation of tailplane icing of a twin-turboprop business transport at Edwards Air Force Base. The flight test was conducted to evaluate ice shape growth and extent of ice on the tailplane for specific weather conditions of Liquid Water Content (LWC), droplet size, and ambient temperature. This work analyzes the flight test data comparing the drag for various tailplane icing conditions with respect to a flight test verified calibrated aircraft model. Although less than a third of the test aircraft was involved in the icing environment, the results of this analysis shows a significant increase in the aircraft drag with respect to the LWC, droplet size, and ambient temperature.

Keywords

Icing, Flight test, Liquid water content, Mean volumetric diameter, Coefficient of drag

Disciplines

Aerospace Engineering | Engineering | Mechanical Engineering

License

This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.

Comments

Degree granted by The University of Texas at Arlington

Recommended Citation

Shaikh, Shehzad Maksudahmad, "Analysis of an Artificial Tailplane Icing Flight Test of a High-Wing, Twin-Engine Aircraft" (2016). Mechanical and Aerospace Engineering Theses. 750.
https://mavmatrix.uta.edu/mechaerospace_theses/750