Professional Course Module
T&E 4111 – Helicopter Performance Flight Testing I 
(3 Credits)


Course Description
    An intensive overview of the analytical theory and procedures used to evaluate performance characteristics of helicopters. Emphasis is placed on subsonic aerodynamics, rotor blade aerodynamics, pitot static system performance, hover performance, vertical climb performance and level flight performance.

Texts and Reference Materials
    “Helicopter Performance, Stability and Control,” R. W. Prouty
    NTPS Course Notes

Anticipated Student Learning Objectives
    Upon successful completion of this course of instruction, the student will have a basic understanding of performance flight test procedures, techniques, and data analysis. He/she will:
Be familiar with
    1.  The aerodynamics of a rotating blade.
    2.  Hover performance theory, requirements and flight-test techniques.
    3.  Vertical climb performance theory, requirements and flight-test techniques.
    4. Level flight performance theory, requirements and flight-test techniques.
Understand
    5.  Dimensional analysis and be able to perform dimensional calculations.
    6.  Basic subsonic aerodynamics.
    7.  Pitot-static theory and be familiar with the Standard Atmosphere.
 
Sequence of Instruction
Performance Testing Overview 
Dimensional Analysis 
Subsonic Aerodynamics 
Rotor Blade Aerodynamics 
Pitot-Static Theory 
Position Error Correction (PEC) Requirements and Flight Test Techniques 
Hover Performance Theory and Flight Test Techniques 
Vertical Climb Performance Theory and Flight Test Techniques 
Level Flight Theory and Flight Test Techniques 
Tutorials -  Aerodynamics, Pitot-Statics, Helicopter Performance 
Exams - Aerodynamics, Pitot-Statics, Helicopter Performance
Instructional Methodology
Lectures.

Process of Evaluation
Written Examinations.


 


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