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 ESDU
 AERO
 F.08.01.02
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ESDU AERO F.08.01.02 49th Edition, November 1, 2003
Increment to C sub m sub zero due to flaps on swept-back wings.
Includes all amendments and changes through AC, November 1, 2003

ESDU AERO F.08.01.02

49th Edition, November 1, 2003

Complete Document
 
Increment to C sub m sub zero due to flaps on swept-back wings.
Includes all amendments and changes through AC, November 1, 2003
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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.02.01.08 45th Edition, October 1, 2013
VORTEX DRAG COEFFICIENT OF WING WITH PART-SPAN FLAP AND CENTRAL CUT-OUT
Includes all amendments and changes through AE, October 1, 2013

ESDU AERO F.02.01.08

45th Edition, October 1, 2013

Complete Document
 
VORTEX DRAG COEFFICIENT OF WING WITH PART-SPAN FLAP AND CENTRAL CUT-OUT
Includes all amendments and changes through AE, October 1, 2013
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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 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 AERO F.02.01.07 44th Edition, February 1, 1993
Conversion factor for profile drag increment for part-span flaps.
Includes all amendments and changes through AC, February 1, 1993

ESDU AERO F.02.01.07

44th Edition, February 1, 1993

Complete Document
 
Conversion factor for profile drag increment for part-span flaps.
Includes all amendments and changes through AC, February 1, 1993
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ESDU AERO A.08.01.05 53rd Edition, January 1, 2007
Aerodynamic centre in two-dimensional flow.
Includes all amendments and changes through AB, January 1, 2007

ESDU AERO A.08.01.05

53rd Edition, January 1, 2007

Complete Document
 
Aerodynamic centre in two-dimensional flow.
Includes all amendments and changes through AB, January 1, 2007
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ESDU AERO A.08.01.09 58th Edition, February 1, 1981
Flow field of subsonic axisymmetric jet in a parallel stream.
Includes all amendments and changes through AA, February 1, 1981

ESDU AERO A.08.01.09

58th Edition, February 1, 1981

Complete Document
 
Flow field of subsonic axisymmetric jet in a parallel stream.
Includes all amendments and changes through AA, February 1, 1981
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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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Additional Comments:
POA * ONLINE SUBSCRIPTION ONLY
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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 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 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 STRUCT 02.01.02 47th Edition, August 1, 1977
Average and edge stresses for long flat plates in compression for different edge conditions.
Includes all amendments and changes through AA, August 1, 1977

ESDU STRUCT 02.01.02

47th Edition, August 1, 1977

Complete Document
 
Average and edge stresses for long flat plates in compression for different edge conditions.
Includes all amendments and changes through AA, August 1, 1977
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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 STRUCT 02.01.08 62nd Edition, November 1, 1990
Buckling in compression of sheet between rivets.
Includes all amendments and changes through AC, November 1, 1990

ESDU STRUCT 02.01.08

62nd Edition, November 1, 1990

Complete Document
 
Buckling in compression of sheet between rivets.
Includes all amendments and changes through AC, November 1, 1990
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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.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 B.S.02.03.08 54th Edition, January 1, 1980
Forebody-afterbody interference wave drag of simple pointed or ducted body shapes with short midbodies.
Includes all amendments and changes through AA, January 1, 1980

ESDU AERO B.S.02.03.08

54th Edition, January 1, 1980

Complete Document
 
Forebody-afterbody interference wave drag of simple pointed or ducted body shapes with short midbodies.
Includes all amendments and changes through AA, January 1, 1980
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ESDU AERO W.S.08.03.02 57th Edition, March 1, 1982
Pitching velocity derivatives for wings at supersonic speeds Z sub q and M sub q.
Includes all amendments and changes through AB, March 1, 1982

ESDU AERO W.S.08.03.02

57th Edition, March 1, 1982

Complete Document
 
Pitching velocity derivatives for wings at supersonic speeds Z sub q and M sub q.
Includes all amendments and changes through AB, March 1, 1982
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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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