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 ESDU
 AERO
 W.05.01.01
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ESDU AERO W.05.01.01 48th Edition, March 1, 1981
Kinetic pressure in the wake behind a wing.
Includes all amendments and changes through AA, March 1, 1981

ESDU AERO W.05.01.01

48th Edition, March 1, 1981

Complete Document
 
Kinetic pressure in the wake behind a wing.
Includes all amendments and changes through AA, March 1, 1981
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ESDU AERO F.05.01.01 50th Edition, December 1, 1973
Normal force on flaps and controls.
Includes all amendments and changes through AA, December 1, 1973

ESDU AERO F.05.01.01

50th Edition, December 1, 1973

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Normal force on flaps and controls.
Includes all amendments and changes through AA, December 1, 1973
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ESDU AERO W.01.01.05 55th Edition, August 1, 2007
Slope of lift curve for two-dimensional flow.
Includes all amendments and changes through AE, August 1, 2007

ESDU AERO W.01.01.05

55th Edition, August 1, 2007

Complete Document
 
Slope of lift curve for two-dimensional flow.
Includes all amendments and changes through AE, August 1, 2007
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ESDU AERO W.01.01.04 46th Edition, May 1, 1974
Effect of cut-out on lift-curve slope.
Includes all amendments and changes through AA, May 1, 1974

ESDU AERO W.01.01.04

46th Edition, May 1, 1974

Complete Document
 
Effect of cut-out on lift-curve slope.
Includes all amendments and changes through AA, May 1, 1974
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ESDU AERO W.01.01.07 54th Edition, September 1, 1985
Maximum lift coefficients for aerofoil sections at Mach numbers from 0.60. to 0.75.
Includes all amendments and changes through AB, September 1, 1985

ESDU AERO W.01.01.07

54th Edition, September 1, 1985

Complete Document
 
Maximum lift coefficients for aerofoil sections at Mach numbers from 0.60. to 0.75.
Includes all amendments and changes through AB, September 1, 1985
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ESDU AERO W.S.05.03.01 56th Edition, January 1, 1994
Pressure distribution on blunt noses of two-dimensional sections at zero incidence in supersonic flow.
Includes all amendments and changes through AB, January 1, 1994

ESDU AERO W.S.05.03.01

56th Edition, January 1, 1994

Complete Document
 
Pressure distribution on blunt noses of two-dimensional sections at zero incidence in supersonic flow.
Includes all amendments and changes through AB, January 1, 1994
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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 AERO W.02.04.01 47th Edition, July 1, 1973
Drag of a smooth flat plate at zero incidence.
Includes all amendments and changes through AB, July 1, 1973

ESDU AERO W.02.04.01

47th Edition, July 1, 1973

Complete Document
 
Drag of a smooth flat plate at zero incidence.
Includes all amendments and changes through AB, July 1, 1973
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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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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 C.01.01.03 56th Edition, May 1, 1978
Rate of change of lift coefficient with control deflection in incompressible two-dimensional flow, (a sub 2) sub zero.
Includes all amendments and changes through AB, May 1, 1978

ESDU AERO C.01.01.03

56th Edition, May 1, 1978

Complete Document
 
Rate of change of lift coefficient with control deflection in incompressible two-dimensional flow, (a sub 2) sub zero.
Includes all amendments and changes through AB, May 1, 1978
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ESDU AERO C.01.01.01 1982 Edition, April 1, 1982
Lift-curve slope for single fin and rudder. (i) Body shape merging into fin.
Includes all amendments and changes through AB, April 1, 1982

ESDU AERO C.01.01.01

1982 Edition, April 1, 1982

Complete Document
 
Lift-curve slope for single fin and rudder. (i) Body shape merging into fin.
Includes all amendments and changes through AB, April 1, 1982
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ESDU AERO C.04.01.01 56th Edition, August 1, 1989
Rate of change of hinge-moment coefficient with incidence for a plain control in incompressible two-dimensional flow, (b sub 1) sub zero.
Includes all amendments and changes through AB, August 1, 1989

ESDU AERO C.04.01.01

56th Edition, August 1, 1989

Complete Document
 
Rate of change of hinge-moment coefficient with incidence for a plain control in incompressible two-dimensional flow, (b sub 1) sub zero.
Includes all amendments and changes through AB, August 1, 1989
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ESDU AERO F.01.01.09 48th Edition, August 1, 1995
Lift coefficient increment due to full-span double flap (main flap slotted).
Includes all amendments and changes through AC, August 1, 1995

ESDU AERO F.01.01.09

48th Edition, August 1, 1995

Complete Document
 
Lift coefficient increment due to full-span double flap (main flap slotted).
Includes all amendments and changes through AC, August 1, 1995
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ESDU AERO A.06.01.01 1981 Edition, March 1, 1981
Stability derivative L sub p, rolling moment due to rolling for swept and tapered wings.
Includes all amendments and changes through AA, March 1, 1981

ESDU AERO A.06.01.01

1981 Edition, March 1, 1981

Complete Document
 
Stability derivative L sub p, rolling moment due to rolling for swept and tapered wings.
Includes all amendments and changes through AA, March 1, 1981
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ESDU AERO C.01.01.04 48th Edition, March 1, 1980
Effect of gap on the slope of lift curve and slope of lift increment curve due to control surface deflection.
Includes all amendments and changes through AA, March 1, 1980

ESDU AERO C.01.01.04

48th Edition, March 1, 1980

Complete Document
 
Effect of gap on the slope of lift curve and slope of lift increment curve due to control surface deflection.
Includes all amendments and changes through AA, March 1, 1980
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ESDU AERO F.01.01.08 49th Edition, December 1, 2014
LIFT COEFFICIENT INCREMENT DUE TO FULL-SPAN SLOTTED FLAPS
Includes all amendments and changes through Addendum , December 1, 2014

ESDU AERO F.01.01.08

49th Edition, December 1, 2014

Complete Document
 
LIFT COEFFICIENT INCREMENT DUE TO FULL-SPAN SLOTTED FLAPS
Includes all amendments and changes through Addendum , December 1, 2014
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ESDU AERO C.08.01.01 56th Edition, August 1, 2015
RATE OF CHANGE OF PITCHING MOMENT COEFFICIENT WITH CONTROL DEFLECTION FOR A PLAIN CONTROL IN INCOMPRESSIBLE TWO-DIMENSIONAL FLOW, m sub zero
Includes all amendments and changes through AB, August 1, 2015

ESDU AERO C.08.01.01

56th Edition, August 1, 2015

Complete Document
 
RATE OF CHANGE OF PITCHING MOMENT COEFFICIENT WITH CONTROL DEFLECTION FOR A PLAIN CONTROL IN INCOMPRESSIBLE TWO-DIMENSIONAL FLOW, m sub zero
Includes all amendments and changes through AB, August 1, 2015
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ESDU AERO F.08.01.01 48th Edition, November 1, 2003
Pitching moment coefficient increment due to flaps for unswept wings.
Includes all amendments and changes through Addendum , November 1, 2003

ESDU AERO F.08.01.01

48th Edition, November 1, 2003

Complete Document
 
Pitching moment coefficient increment due to flaps for unswept wings.
Includes all amendments and changes through Addendum , November 1, 2003
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ESDU AERO W.02.04.11 43rd Edition, December 1, 1974
Limit of surface waviness for laminar flow over wings.
Includes all amendments and changes through AB, December 1, 1974

ESDU AERO W.02.04.11

43rd Edition, December 1, 1974

Complete Document
 
Limit of surface waviness for laminar flow over wings.
Includes all amendments and changes through AB, December 1, 1974
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