17,005 Documents in our Technical Library
2449947 Total Downloads

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

AEDC-TR-76-16

  • Version
  • 223 Downloads
  • 30.69 MB File Size
  • 1 File Count
  • March 1, 2017 Create Date
  • March 1, 2017 Last Updated
Scroll for Details

Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine

A set of tables is presented that contain several thermodynamic 
properties of air and the exhaust gas from a turbine engine. 
The tables were assembled to provide a readily available source 
of thermodynamic properties routinely used in hand calculations of turbine 
engine data. The properties include enthalpy, entropy, and specific heat 
at constant pressure. The properties were calculated using an air com- 
position from Ref. 1 but modified to reduce the number of constituents to 
five for reduced computer calculation time. The composition used in 
these calculations is given as follows:
The molecular weight for this composition was defined as 28. 9646. 
to represent the J P -4 grade of fuel currently in use in turbine engines. 
The fuel composition was defined as CnH1. 95n 
The range of air properties is from 300 to 18000 R, and the 
pressure range is from O. 5 to 600 psia. The data are tabulated in 
temperature increments of IOOR and graduated pressure steps of O. 5 
to 100 psia. 
The data for exhaust gas ranges from a temperature of 600 to 
40000R, from a pressure of O. 5 to 600 psia, and a fuel-to-air ratio of 
O. 005 to O. 067. The temperature increments are for enthalpy 
and 1000R for entropy and specific heat. 
The properties were calculated using the method of Ref. 2. 
The thermodynamic properties of the constituent gases were taken 
from Ref. 3 (argon and neon properties were taken from Ref. 4). 
Real gas effects were included in the calculation of the air properties

 

FileAction
AEDC-TR-76-16 Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

AEDC-TR-76-16

  • Version
  • 223 Downloads
  • 30.69 MB File Size
  • 1 File Count
  • March 1, 2017 Create Date
  • March 1, 2017 Last Updated
Scroll for Details

Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine

A set of tables is presented that contain several thermodynamic 
properties of air and the exhaust gas from a turbine engine. 
The tables were assembled to provide a readily available source 
of thermodynamic properties routinely used in hand calculations of turbine 
engine data. The properties include enthalpy, entropy, and specific heat 
at constant pressure. The properties were calculated using an air com- 
position from Ref. 1 but modified to reduce the number of constituents to 
five for reduced computer calculation time. The composition used in 
these calculations is given as follows:
The molecular weight for this composition was defined as 28. 9646. 
to represent the J P -4 grade of fuel currently in use in turbine engines. 
The fuel composition was defined as CnH1. 95n 
The range of air properties is from 300 to 18000 R, and the 
pressure range is from O. 5 to 600 psia. The data are tabulated in 
temperature increments of IOOR and graduated pressure steps of O. 5 
to 100 psia. 
The data for exhaust gas ranges from a temperature of 600 to 
40000R, from a pressure of O. 5 to 600 psia, and a fuel-to-air ratio of 
O. 005 to O. 067. The temperature increments are for enthalpy 
and 1000R for entropy and specific heat. 
The properties were calculated using the method of Ref. 2. 
The thermodynamic properties of the constituent gases were taken 
from Ref. 3 (argon and neon properties were taken from Ref. 4). 
Real gas effects were included in the calculation of the air properties

 

FileAction
AEDC-TR-76-16 Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine.pdfDownload 
17,005 Documents in our Technical Library
2449947 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...