CNATRA P-201: Aircraft Engines and Systems | T.REX ARMS Field Manual Vault

CNATRA P-201 Aircraft Engines and Systems

CNATRA P-201

Aircraft Engines and Systems

Navy · CNATRA · May 2001 · 171 pages

About

This assignment will aid the student in understanding the principles of operation for a gas turbine engine. LESSON TOPIC LEARNING OBJECTIVES Terminal Objective: Partially supported by this lesson topic: 3.0 Upon completion of this unit of instruction, the student will demonstrate knowledge of the fundamentals of power plants and associated accessory systems. Enabling Objectives: Completely supported by this lesson topic: 3.1 Explain the relationship between static pressure, dynamic pressure and total pressure. 3.2 State Bernoulli's Theorem. 3.3 Describe the behavior of subsonic airflow in a nozzle and diffuser. 3.4 Describe the behavior of supersonic airflow in a nozzle and diffuser. 3.5 Identify the three main sections of a gas generator. 3.6 Describe the Brayton Cycle. 3.7 Describe the basic components and operation of the gas generator.

DesignationCNATRA P-201

EditionMay 2001

StatusSuperseded

Pages171

FunctionAviation

CollectionRecent Archive

No distribution statement on the cover; no restrictive marking found

References 3

JP 4Not in the Vault
JP 5Not in the Vault
JP 8Not in the Vault