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 ESDU
 AERO
 C.01.01.04
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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 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 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 C.04.01.04 49th Edition, September 1, 1994
Effect of Irving internal balance on hinge-moment coefficient in two-dimensional flow.
Includes all amendments and changes through AC, September 1, 1994

ESDU AERO C.04.01.04

49th Edition, September 1, 1994

Complete Document
 
Effect of Irving internal balance on hinge-moment coefficient in two-dimensional flow.
Includes all amendments and changes through AC, September 1, 1994
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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 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 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 C.04.01.03 49th Edition, August 1, 1989
Effect of nose balance on two-dimensional control hinge-moment coefficients.
Includes all amendments and changes through AB, August 1, 1989

ESDU AERO C.04.01.03

49th Edition, August 1, 1989

Complete Document
 
Effect of nose balance on two-dimensional control hinge-moment coefficients.
Includes all amendments and changes through AB, August 1, 1989
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ESDU AERO C.04.01.02 56th Edition, August 1, 1989
Rate of change of hinge-moment coefficient with control deflection for a plain control in incompressible two-dimensional flow, (b sub 2) sub zero.
Includes all amendments and changes through AB, August 1, 1989

ESDU AERO C.04.01.02

56th Edition, August 1, 1989

Complete Document
 
Rate of change of hinge-moment coefficient with control deflection for a plain control in incompressible two-dimensional flow, (b sub 2) sub zero.
Includes all amendments and changes through AB, August 1, 1989
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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 C.04.01.08 48th Edition, August 1, 1989
Control hinge-moment coefficient derivative due to tab.
Includes all amendments and changes through AB, August 1, 1989

ESDU AERO C.04.01.08

48th Edition, August 1, 1989

Complete Document
 
Control hinge-moment coefficient derivative due to tab.
Includes all amendments and changes through AB, August 1, 1989
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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 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 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 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 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

Complete Document
 
Normal force on flaps and controls.
Includes all amendments and changes through AA, December 1, 1973
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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 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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