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 ESDU
 AERO
 C.04.01.06
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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.04.01.04 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.04.01.03 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.04.01.01 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.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 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 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 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 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 STRUCT 02.04.01 43rd Edition, March 1, 1976
Buckling stress ratios for plates under uniform compression and shear.
Includes all amendments and changes through AA, March 1, 1976

ESDU STRUCT 02.04.01

43rd Edition, March 1, 1976

Complete Document
 
Buckling stress ratios for plates under uniform compression and shear.
Includes all amendments and changes through AA, March 1, 1976
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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

Complete Document
 
Form factors for circular sections under combined bending and axial load.
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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 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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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.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.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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POA * ONLINE SUBSCRIPTION ONLY
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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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