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 ESDU
 AERO
 00.03.05
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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

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Isentropic expansion of air from rest.
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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

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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

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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

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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 AERO W.S.00.03.05 56th Edition, October 1, 1982
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO W.S.00.03.05

56th Edition, October 1, 1982

Complete Document
 
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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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

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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 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 00.01.06 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 S.00.03.16 54th Edition, March 1, 1975
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on wedges.
Includes all amendments and changes through AB, March 1, 1975

ESDU AERO S.00.03.16

54th Edition, March 1, 1975

Complete Document
 
Conditions for shock wave detachment and for subsonic flow behind nose shock waves on cones at zero incidence and on wedges.
Includes all amendments and changes through AB, March 1, 1975
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ESDU AERO S.00.03.23 59th Edition, June 1, 1982
Conditions behind oblique shock waves for air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982

ESDU AERO S.00.03.23

59th Edition, June 1, 1982

Complete Document
 
Conditions behind oblique shock waves for air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982
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ESDU AERO S.00.03.22 59th Edition, June 1, 1982
Conditions behind normal shock waves in air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982

ESDU AERO S.00.03.22

59th Edition, June 1, 1982

Complete Document
 
Conditions behind normal shock waves in air in dissociation equilibrium.
Includes all amendments and changes through AA, June 1, 1982
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ESDU AERO S.00.03.14 53rd Edition, March 1, 1995
Approximate calculation of the pressure changes in two-dimensional supersonic flow.
Includes all amendments and changes through AB, March 1, 1995

ESDU AERO S.00.03.14

53rd Edition, March 1, 1995

Complete Document
 
Approximate calculation of the pressure changes in two-dimensional supersonic flow.
Includes all amendments and changes through AB, March 1, 1995
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ESDU AERO S.00.03.13 54th Edition, May 1, 1975
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones.
Includes all amendments and changes through AB, May 1, 1975

ESDU AERO S.00.03.13

54th Edition, May 1, 1975

Complete Document
 
Inviscid supersonic flow past cones at zero incidence: (ii) surface pressure coefficient and shock angle for circular cones.
Includes all amendments and changes through AB, May 1, 1975
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ESDU AERO S.00.03.27 63rd Edition, November 1, 1979
Examples in the use of the Mollier chart (isentropic flow and Prandtl-Meyer expansion for air in dissociation equilibrium).
Includes all amendments and changes through AA, November 1, 1979

ESDU AERO S.00.03.27

63rd Edition, November 1, 1979

Complete Document
 
Examples in the use of the Mollier chart (isentropic flow and Prandtl-Meyer expansion for air in dissociation equilibrium).
Includes all amendments and changes through AA, November 1, 1979
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ESDU AERO S.00.03.15 Revision B, December 1, 1977
Pitot and static tubes in supersonic flow.
Includes all amendments and changes through AB, December 1, 1977

ESDU AERO S.00.03.15

Revision B, December 1, 1977

Complete Document
 
Pitot and static tubes in supersonic flow.
Includes all amendments and changes through AB, December 1, 1977
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