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ESDU 06014 2006 Edition, August 1, 2006
Zero-lift drag coefficient increment due to full-span plain flaps.

ESDU 06014

2006 Edition, August 1, 2006

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Zero-lift drag coefficient increment due to full-span plain flaps.
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ESDU 88029 88th Edition, November 1, 2006
Yawing moment coefficient for plain ailerons at subsonic speeds.
Includes all amendments and changes through AC, November 1, 2006

ESDU 88029

88th Edition, November 1, 2006

Complete Document
 
Yawing moment coefficient for plain ailerons at subsonic speeds.
Includes all amendments and changes through AC, November 1, 2006
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ESDU 88032 88th Edition, October 1, 1991
Wrinkling of sandwich panel face plates (isotropic face plates on orthotropic cores, in-plane loading or bending).
Includes all amendments and changes through AA, October 1, 1991

ESDU 88032

88th Edition, October 1, 1991

Complete Document
 
Wrinkling of sandwich panel face plates (isotropic face plates on orthotropic cores, in-plane loading or bending).
Includes all amendments and changes through AA, October 1, 1991
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ESDU 88037 2012 Edition, February 1, 2012
World-wide extreme wind speeds. Part 2: examples using various methods of analysis

ESDU 88037

2012 Edition, February 1, 2012

Complete Document
 
World-wide extreme wind speeds. Part 2: examples using various methods of analysis
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ESDU 87034 2012 Edition, February 1, 2012
World-wide extreme wind speeds Part 1: origins and methods analysis

ESDU 87034

2012 Edition, February 1, 2012

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World-wide extreme wind speeds Part 1: origins and methods analysis
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ESDU 10004 2013 Edition, September 1, 2015
Worked example of ground-test machine operating on a dry or contaminated runway surface. Application of ESDU 05011
Includes all amendments and changes through AB, September 1, 2015

ESDU 10004

2013 Edition, September 1, 2015

Complete Document
 
Worked example of ground-test machine operating on a dry or contaminated runway surface. Application of ESDU 05011
Includes all amendments and changes through AB, September 1, 2015
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ESDU 15007 2015 Edition, September 1, 2015
Worked example for tyre in yawed motion on a dry or wet runway surface An application of ESDU 13007

ESDU 15007

2015 Edition, September 1, 2015

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Worked example for tyre in yawed motion on a dry or wet runway surface An application of ESDU 13007
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ESDU 10003 2013 Edition, September 1, 2015
Worked example for tyre in linear motion on a contaminated runway surface. An application of ESDU 05011
Includes all amendments and changes through AB, September 1, 2015

ESDU 10003

2013 Edition, September 1, 2015

Complete Document
 
Worked example for tyre in linear motion on a contaminated runway surface. An application of ESDU 05011
Includes all amendments and changes through AB, September 1, 2015
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ESDU 13002 2013 Edition, September 1, 2015
Worked example for aircraft with multiple-wheel undercarriages braking on water-covered runway. Application of ESDU 11004
Includes all amendments and changes through AA, September 1, 2015

ESDU 13002

2013 Edition, September 1, 2015

Complete Document
 
Worked example for aircraft with multiple-wheel undercarriages braking on water-covered runway. Application of ESDU 11004
Includes all amendments and changes through AA, September 1, 2015
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ESDU 07002 2008 Edition, December 1, 2011
Wing viscous drag coefficient in shock-free attached flow
Includes all amendments and changes through AA, December 1, 2011

ESDU 07002

2008 Edition, December 1, 2011

Complete Document
 
Wing viscous drag coefficient in shock-free attached flow
Includes all amendments and changes through AA, December 1, 2011
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ESDU 87001 87th Edition, July 1, 1991
Wing pitching moment at zero lift at subcritical Mach numbers.
Includes all amendments and changes through AB, July 1, 1991

ESDU 87001

87th Edition, July 1, 1991

Complete Document
 
Wing pitching moment at zero lift at subcritical Mach numbers.
Includes all amendments and changes through AB, July 1, 1991
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ESDU 93019 93rd Edition, July 1, 1995
Wing lift increment at zero angle of attack due to deployment of single-slotted flaps at low speeds.
Includes all amendments and changes through AA, July 1, 1995

ESDU 93019

93rd Edition, July 1, 1995

Complete Document
 
Wing lift increment at zero angle of attack due to deployment of single-slotted flaps at low speeds.
Includes all amendments and changes through AA, July 1, 1995
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ESDU TM 169 2012 Edition, March 1, 2012
Wing lift-curve slope in inviscid subsonic flow: Improvements to the Helmbold-Diederich equation and comparison with data from ESDU 70011

ESDU TM 169

2012 Edition, March 1, 2012

Complete Document
 
Wing lift-curve slope in inviscid subsonic flow: Improvements to the Helmbold-Diederich equation and comparison with data from ESDU 70011
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ESDU 97009 97th Edition, November 1, 2003
Wing lift coefficient increment at zero angle of attack due to deployment of trailing-edge split flaps at low speeds.
Includes all amendments and changes through AA, November 1, 2003

ESDU 97009

97th Edition, November 1, 2003

Complete Document
 
Wing lift coefficient increment at zero angle of attack due to deployment of trailing-edge split flaps at low speeds.
Includes all amendments and changes through AA, November 1, 2003
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ESDU 97011 97th Edition, November 1, 2003
Wing lift coefficient increment at zero angle of attack due to deployment of plain trailing-edge flaps at low speeds.
Includes all amendments and changes through AA, November 1, 2003

ESDU 97011

97th Edition, November 1, 2003

Complete Document
 
Wing lift coefficient increment at zero angle of attack due to deployment of plain trailing-edge flaps at low speeds.
Includes all amendments and changes through AA, November 1, 2003
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ESDU 96032 1996 Edition, November 1, 1996
Wing lift coefficient increment at zero angle of attack due to deployment of leading-edge devices at low speeds.

ESDU 96032

1996 Edition, November 1, 1996

Complete Document
 
Wing lift coefficient increment at zero angle of attack due to deployment of leading-edge devices at low speeds.
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ESDU 95021 1995 Edition, August 1, 1995
Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low speeds.

ESDU 95021

1995 Edition, August 1, 1995

Complete Document
 
Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low speeds.
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ESDU 79006 1999 Edition, March 1, 1999
Wing-body yawing moment and sideforce derivatives due to sideslip: N sub v and Y sub v (with Addendum A for nacelle effects).
Includes all amendments and changes through AB, March 1, 1999

ESDU 79006

1999 Edition, March 1, 1999

Complete Document
 
Wing-body yawing moment and sideforce derivatives due to sideslip: N sub v and Y sub v (with Addendum A for nacelle effects).
Includes all amendments and changes through AB, March 1, 1999
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ESDU 87031 87th Edition, January 1, 2013
Wing angle of attack for zero lift at subcritical Mach numbers
Includes all amendments and changes through AC, January 1, 2013

ESDU 87031

87th Edition, January 1, 2013

Complete Document
 
Wing angle of attack for zero lift at subcritical Mach numbers
Includes all amendments and changes through AC, January 1, 2013
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Additional Comments:
POA * ONLINE SUBSCRIPTION ONLY
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ESDU 84011 2012 Edition, February 1, 2012
Wind speed profiles over terrain with roughness changes

ESDU 84011

2012 Edition, February 1, 2012

Complete Document
 
Wind speed profiles over terrain with roughness changes
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