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 AERO
 W.S.05.03.01
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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 AERO B.S.05.03.01 54th Edition, March 1, 1980
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
Includes all amendments and changes through AA, March 1, 1980

ESDU AERO B.S.05.03.01

54th Edition, March 1, 1980

Complete Document
 
Pressure distribution on forebodies and afterbodies of revolution at zero incidence in inviscid flow.
Includes all amendments and changes through AA, March 1, 1980
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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 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.00.03.04 54th Edition, March 1, 1995
Theoretical properties of two-dimensional supersonic aerofoils of simple section.
Includes all amendments and changes through AB, March 1, 1995

ESDU AERO W.S.00.03.04

54th Edition, March 1, 1995

Complete Document
 
Theoretical properties of two-dimensional supersonic aerofoils of simple section.
Includes all amendments and changes through AB, March 1, 1995
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ESDU AERO W.S.02.03.02 57th Edition, October 1, 1982
Theoretical lift-dependent drag of wings at supersonic speeds.
Includes all amendments and changes through AB, October 1, 1982

ESDU AERO W.S.02.03.02

57th Edition, October 1, 1982

Complete Document
 
Theoretical lift-dependent drag of wings at supersonic speeds.
Includes all amendments and changes through AB, October 1, 1982
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ESDU AERO W.S.02.03.10 64th Edition, October 1, 1982
Wave drag of flat plates with blunt noses at zero incidence.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO W.S.02.03.10

64th Edition, October 1, 1982

Complete Document
 
Wave drag of flat plates with blunt noses at zero incidence.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO W.S.00.03.18 55th Edition, January 1, 1981
Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation.
Includes all amendments and changes through AB, January 1, 1981

ESDU AERO W.S.00.03.18

55th Edition, January 1, 1981

Complete Document
 
Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation.
Includes all amendments and changes through AB, January 1, 1981
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ESDU AERO W.S.02.03.09 1955 Edition, February 1, 1955
Transonic drag rise of rectangular symmetrical section wings at zero lift. NACA 65 series sections.

ESDU AERO W.S.02.03.09

1955 Edition, February 1, 1955

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Transonic drag rise of rectangular symmetrical section wings at zero lift. NACA 65 series sections.
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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 W.S.02.03.07 1965 Edition, September 1, 1965
Base pressure on aerofoil sections with a blunt trailing edge in supersonic flow.

ESDU AERO W.S.02.03.07

1965 Edition, September 1, 1965

Complete Document
 
Base pressure on aerofoil sections with a blunt trailing edge in supersonic flow.
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ESDU AERO W.S.00.03.03 56th Edition, October 1, 1982
Introductory Item on two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO W.S.00.03.03

56th Edition, October 1, 1982

Complete Document
 
Introductory Item on two-dimensional aerofoils at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO W.S.02.04.12 56th Edition, May 1, 1983
Skin friction drag coefficients for a flat plate in two-dimensional flow with zero heat transfer.
Includes all amendments and changes through AA, May 1, 1983

ESDU AERO W.S.02.04.12

56th Edition, May 1, 1983

Complete Document
 
Skin friction drag coefficients for a flat plate in two-dimensional flow with zero heat transfer.
Includes all amendments and changes through AA, May 1, 1983
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ESDU AERO W.S.02.04.13 56th Edition, May 1, 1983
Profile drag coefficients for two-dimensional biconvex aerofoil with zero heat transfer at supersonic speeds.
Includes all amendments and changes through AA, May 1, 1983

ESDU AERO W.S.02.04.13

56th Edition, May 1, 1983

Complete Document
 
Profile drag coefficients for two-dimensional biconvex aerofoil with zero heat transfer at supersonic speeds.
Includes all amendments and changes through AA, May 1, 1983
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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.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 A.S.06.03.01 57th Edition, October 1, 1982
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982

ESDU AERO A.S.06.03.01

57th Edition, October 1, 1982

Complete Document
 
Stability derivative L sub p, rolling moment due to rolling for wings at supersonic speeds.
Includes all amendments and changes through AA, October 1, 1982
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ESDU AERO B.S.02.03.01 54th Edition, January 1, 1981
Introductory notes on the drag at zero incidence of bodies at supersonic speeds.
Includes all amendments and changes through AC, January 1, 1981

ESDU AERO B.S.02.03.01

54th Edition, January 1, 1981

Complete Document
 
Introductory notes on the drag at zero incidence of bodies at supersonic speeds.
Includes all amendments and changes through AC, January 1, 1981
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ESDU AERO A.S.02.03.01 59th Edition, May 1, 1975
Explanatory notes on transonic and supersonic area rules.
Includes all amendments and changes through AB, May 1, 1975

ESDU AERO A.S.02.03.01

59th Edition, May 1, 1975

Complete Document
 
Explanatory notes on transonic and supersonic area rules.
Includes all amendments and changes through AB, May 1, 1975
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ESDU STRUCT 07.03.01 64th Edition, April 1, 1974
Sandwich panels with corrugated core and equal face plates. Transverse shear stiffness.
Includes all amendments and changes through AA, April 1, 1974

ESDU STRUCT 07.03.01

64th Edition, April 1, 1974

Complete Document
 
Sandwich panels with corrugated core and equal face plates. Transverse shear stiffness.
Includes all amendments and changes through AA, April 1, 1974
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