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 ESDU
 AERO
 00.01.06
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ESDU AERO 00.01.06 59th Edition, May 1, 1982
Thermodynamic properties of air in dissociation equilibrium.
Includes all amendments and changes through AA, May 1, 1982

ESDU AERO 00.01.06

59th Edition, May 1, 1982

Complete Document
 
Thermodynamic properties of air in dissociation equilibrium.
Includes all amendments and changes through AA, May 1, 1982
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ESDU AERO 00.01.12 62nd Edition, May 1, 1982
Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 100 K to T = 6 000 K.
Includes all amendments and changes through AA, May 1, 1982

ESDU AERO 00.01.12

62nd Edition, May 1, 1982

Complete Document
 
Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 100 K to T = 6 000 K.
Includes all amendments and changes through AA, May 1, 1982
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ESDU AERO 00.01.11 62nd Edition, May 1, 1982
Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 2 000 K to T = 13 000 K.
Includes all amendments and changes through AA, May 1, 1982

ESDU AERO 00.01.11

62nd Edition, May 1, 1982

Complete Document
 
Mollier chart of the thermodynamic properties of argon-free air in dissociation equilibrium: T = 2 000 K to T = 13 000 K.
Includes all amendments and changes through AA, May 1, 1982
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ESDU AERO 00.01.07 61st Edition, July 1, 1972
Approximate transport properties of high-temperature air in dissociation equilibrium.
Includes all amendments and changes through AA, July 1, 1972

ESDU AERO 00.01.07

61st Edition, July 1, 1972

Complete Document
 
Approximate transport properties of high-temperature air in dissociation equilibrium.
Includes all amendments and changes through AA, July 1, 1972
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ESDU AERO 00.01.08 61st Edition, May 1, 1982
Specific heat capacities and their ratio as functions of temperature for several common gases.
Includes all amendments and changes through AA, May 1, 1982

ESDU AERO 00.01.08

61st Edition, May 1, 1982

Complete Document
 
Specific heat capacities and their ratio as functions of temperature for several common gases.
Includes all amendments and changes through AA, May 1, 1982
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ESDU AERO 00.01.09 62nd Edition, April 1, 1975
A simple model of a thermally perfect, calorically imperfect diatomic gas. Comparison with real gases.
Includes all amendments and changes through AA, April 1, 1975

ESDU AERO 00.01.09

62nd Edition, April 1, 1975

Complete Document
 
A simple model of a thermally perfect, calorically imperfect diatomic gas. Comparison with real gases.
Includes all amendments and changes through AA, April 1, 1975
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ESDU AERO 00.03.28 63rd Edition, February 1, 1978
Conditions behind normal shock waves in a perfect gas for various values of gamma.
Includes all amendments and changes through AA, February 1, 1978

ESDU AERO 00.03.28

63rd Edition, February 1, 1978

Complete Document
 
Conditions behind normal shock waves in a perfect gas for various values of gamma.
Includes all amendments and changes through AA, February 1, 1978
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ESDU AERO 00.03.26 62nd Edition, April 1, 1973
Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section.
Includes all amendments and changes through AA, April 1, 1973

ESDU AERO 00.03.26

62nd Edition, April 1, 1973

Complete Document
 
Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section.
Includes all amendments and changes through AA, April 1, 1973
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ESDU AERO 00.03.31 1965 Edition, August 1, 1965
Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum flow deflection angle.

ESDU AERO 00.03.31

1965 Edition, August 1, 1965

Complete Document
 
Solutions to the Prandtl-Meyer expansion relations for a range of specific heat ratios: pressure coefficient and maximum flow deflection angle.
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ESDU AERO 00.03.30 65th Edition, January 1, 1999
Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle.
Includes all amendments and changes through AA, January 1, 1999

ESDU AERO 00.03.30

65th Edition, January 1, 1999

Complete Document
 
Solutions to the oblique shock wave relations for a range of specific heat ratios: pressure coefficient and detachment angle.
Includes all amendments and changes through AA, January 1, 1999
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ESDU STRUCT 01.06.00 1956 Edition, November 1, 1956
Information on the use of data sheets 01.06.

ESDU STRUCT 01.06.00

1956 Edition, November 1, 1956

Complete Document
 
Information on the use of data sheets 01.06.
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ESDU AERO 00.03.05 1948 Edition, February 1, 1948
Isentropic expansion of air from rest.

ESDU AERO 00.03.05

1948 Edition, February 1, 1948

Complete Document
 
Isentropic expansion of air from rest.
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ESDU AERO 00.02.05 62nd Edition, February 1, 1981
Heat transfer under conditions of forced convection for the subsonic turbulent flow of gases in smooth straight ducts of constant cross section.
Includes all amendments and changes through AA, February 1, 1981

ESDU AERO 00.02.05

62nd Edition, February 1, 1981

Complete Document
 
Heat transfer under conditions of forced convection for the subsonic turbulent flow of gases in smooth straight ducts of constant cross section.
Includes all amendments and changes through AA, February 1, 1981
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ESDU AERO F.02.01.06 44th Edition, August 1, 2006
Profile drag coefficient increment due to full-span single-slotted flaps (Handley Page and NACA types).
Includes all amendments and changes through AB, August 1, 2006

ESDU AERO F.02.01.06

44th Edition, August 1, 2006

Complete Document
 
Profile drag coefficient increment due to full-span single-slotted flaps (Handley Page and NACA types).
Includes all amendments and changes through AB, August 1, 2006
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ESDU AERO C.04.01.06 49th Edition, August 1, 1989
Full-span control hinge-moment coefficient derivatives for unswept wings in incompressible flow with allowance for spanwise variation of sectional properties.
Includes all amendments and changes through AB, August 1, 1989

ESDU AERO C.04.01.06

49th Edition, August 1, 1989

Complete Document
 
Full-span control hinge-moment coefficient derivatives for unswept wings in incompressible flow with allowance for spanwise variation of sectional properties.
Includes all amendments and changes through AB, August 1, 1989
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ESDU AERO A.06.01.00 58th Edition, January 1, 2015
Information on the use of Data Items on rolling moment derivatives of an aircraft
Includes all amendments and changes through AK, January 1, 2015

ESDU AERO A.06.01.00

58th Edition, January 1, 2015

Complete Document
 
Information on the use of Data Items on rolling moment derivatives of an aircraft
Includes all amendments and changes through AK, January 1, 2015
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ESDU AERO S.00.01.10 62nd Edition, October 1, 1971
One-dimensional isentropic flow of a thermally perfect, calorically imperfect diatomic gas.
Includes all amendments and changes through AA, October 1, 1971

ESDU AERO S.00.01.10

62nd Edition, October 1, 1971

Complete Document
 
One-dimensional isentropic flow of a thermally perfect, calorically imperfect diatomic gas.
Includes all amendments and changes through AA, October 1, 1971
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ESDU STRUCT 01.06.01 1956 Edition, October 1, 1956
Form factors for circular sections under combined bending and axial load.

ESDU STRUCT 01.06.01

1956 Edition, October 1, 1956

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Form factors for circular sections under combined bending and axial load.
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ESDU STRUCT 01.06.02 1956 Edition, October 1, 1956
Form factors for flanged sections under combined bending and axial load.

ESDU STRUCT 01.06.02

1956 Edition, October 1, 1956

Complete Document
 
Form factors for flanged sections under combined bending and axial load.
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ESDU STRUCT 01.06.03 1956 Edition, October 1, 1956
Form factors for angle, tee and channel sections under combined bending and axial load.

ESDU STRUCT 01.06.03

1956 Edition, October 1, 1956

Complete Document
 
Form factors for angle, tee and channel sections under combined bending and axial load.
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