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 ESDU
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 A.00.01
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ESDU FAT A.00.01 58th Edition, February 1, 1975
The effect of mean stress on fatigue strength (plain test piece).
Includes all amendments and changes through AA, February 1, 1975

ESDU FAT A.00.01

58th Edition, February 1, 1975

Complete Document
 
The effect of mean stress on fatigue strength (plain test piece).
Includes all amendments and changes through AA, February 1, 1975
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ESDU FAT A.00.02 58th Edition, April 1, 1973
The effect of mean stress on fatigue strength (test piece with stress concentration).
Includes all amendments and changes through AA, April 1, 1973

ESDU FAT A.00.02

58th Edition, April 1, 1973

Complete Document
 
The effect of mean stress on fatigue strength (test piece with stress concentration).
Includes all amendments and changes through AA, April 1, 1973
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ESDU STRUCT 01.00.01 43rd Edition, April 1, 1980
Flexural properties of stringer sections (lipped and unlipped angles, channels and Z-sections).
Includes all amendments and changes through AA, April 1, 1980

ESDU STRUCT 01.00.01

43rd Edition, April 1, 1980

Complete Document
 
Flexural properties of stringer sections (lipped and unlipped angles, channels and Z-sections).
Includes all amendments and changes through AA, April 1, 1980
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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 FAT A.05.02 65th Edition, April 1, 1973
Estimation of endurance of pin joints.
Includes all amendments and changes through AB, April 1, 1973

ESDU FAT A.05.02

65th Edition, April 1, 1973

Complete Document
 
Estimation of endurance of pin joints.
Includes all amendments and changes through AB, April 1, 1973
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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 00.01.06 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 00.01.09 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 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 FAT E.05.01 58th Edition, April 1, 1977
Endurance of structural joints. (Aluminium alloy material - tensile loading.)
Includes all amendments and changes through AA, April 1, 1977

ESDU FAT E.05.01

58th Edition, April 1, 1977

Complete Document
 
Endurance of structural joints. (Aluminium alloy material - tensile loading.)
Includes all amendments and changes through AA, April 1, 1977
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ESDU FAT E.07.01 62nd Edition, March 1, 1993
Endurance of aluminium alloys (unclad) (in bending).
Includes all amendments and changes through AB, March 1, 1993

ESDU FAT E.07.01

62nd Edition, March 1, 1993

Complete Document
 
Endurance of aluminium alloys (unclad) (in bending).
Includes all amendments and changes through AB, March 1, 1993
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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 A.07.01.00 46th Edition, January 1, 2015
Information on the use of Data Items on yawing moment and sideforce derivatives of an aircraft
Includes all amendments and changes through AI, January 1, 2015

ESDU AERO A.07.01.00

46th Edition, January 1, 2015

Complete Document
 
Information on the use of Data Items on yawing moment and sideforce derivatives of an aircraft
Includes all amendments and changes through AI, January 1, 2015
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ESDU STRUCT 00.07.01 47th Edition, January 1, 1983
Torsion and secondary warping constants for a bulb angle.
Includes all amendments and changes through AA, January 1, 1983

ESDU STRUCT 00.07.01

47th Edition, January 1, 1983

Complete Document
 
Torsion and secondary warping constants for a bulb angle.
Includes all amendments and changes through AA, January 1, 1983
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ESDU STRUCT 00.06.01 44th Edition, December 1, 1980
Method of calculating stress distribution in a reinforced symmetrical shell under bending.
Includes all amendments and changes through AA, December 1, 1980

ESDU STRUCT 00.06.01

44th Edition, December 1, 1980

Complete Document
 
Method of calculating stress distribution in a reinforced symmetrical shell under bending.
Includes all amendments and changes through AA, December 1, 1980
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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 C.04.01.00 50th Edition, August 1, 1989
Introduction to Data Items on control hinge moments.
Includes all amendments and changes through AC, August 1, 1989

ESDU AERO C.04.01.00

50th Edition, August 1, 1989

Complete Document
 
Introduction to Data Items on control hinge moments.
Includes all amendments and changes through AC, August 1, 1989
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ESDU AERO W.00.03.01 53rd Edition, January 1, 1994
Critical Mach number for high speed aerofoil sections.
Includes all amendments and changes through AB, January 1, 1994

ESDU AERO W.00.03.01

53rd Edition, January 1, 1994

Complete Document
 
Critical Mach number for high speed aerofoil sections.
Includes all amendments and changes through AB, January 1, 1994
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