Analysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning / by Melvin S. Feder and Richard Hood.

Format:

Book

Government document

Author/Creator:

Feder, Melvin S., author.

Hood, Richard, author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 2183.

Technical notes / National Advisory Committee for Aeronautics ; No. 2183

Language:

English

Subjects (All):

Airplanes--Control systems.

Airplanes.

Airplanes--Turbine-propeller engines.

Airplanes--Turbofan engines--Afterburners.

Mathematical analysis.

Transfer functions.

Physical Description:

1 online resource (39 pages) : illustrations

Place of Publication:

Washington [D.C.] : National Advisory Committee for Aeronautics, 1950.

Summary:

The analysis was applied to determine the response of turbine-outlet temperature to step changes in the independent variables and was also applied to scheduled and noninteracting control systems.

The general form of transfer functions for a turbojet engine with tail-pipe burining was developed and relations among the coefficient and time constants in these functions were developed from engine thermodynamics and the transfer functions. By means of these relations, the dynamic characteristics of the engine can be found from steady-state data and one transient relation.

Notes:

Title from title screen (viewed June 7, 2019).

"September 1950."

"Lewis Flight Propulsion Laboratory, Cleveland, Ohio."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 35).

Print version record.

Other Format:

Print version: Feder, Melvin S. Analysis for control application of dynamic characteristics of turbojet engine with tail-pipe burning /

OCLC:

1104148323