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ESDU AERO W.02.04.02 1947 Edition, July 1, 1947
Profile drag of smooth wings.

ESDU AERO W.02.04.02

1947 Edition, July 1, 1947

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Profile drag of smooth wings.
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W/D S/S BY ESDU 00027
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ESDU AERO 00.03.05 1948 Edition, February 1, 1948
Isentropic expansion of air from rest.

ESDU AERO 00.03.05

1948 Edition, February 1, 1948

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Isentropic expansion of air from rest.
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ESDU STRUCT 03.06.14 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated radial loads.

ESDU STRUCT 03.06.14

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated radial loads.
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ESDU STRUCT 03.06.13 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Shear forces in a frame due to tangential loads.

ESDU STRUCT 03.06.13

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Shear forces in a frame due to tangential loads.
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ESDU STRUCT 03.06.11 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated radial loads.

ESDU STRUCT 03.06.11

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated radial loads.
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ESDU STRUCT 03.06.09 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated couples.

ESDU STRUCT 03.06.09

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated couples.
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ESDU STRUCT 03.06.07 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Moments in a frame due to concentrated tangential loads.

ESDU STRUCT 03.06.07

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Moments in a frame due to concentrated tangential loads.
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ESDU STRUCT 03.06.12 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated couples.

ESDU STRUCT 03.06.12

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Shear forces in a frame due to concentrated couples.
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ESDU STRUCT 03.06.10 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated tangential loads.

ESDU STRUCT 03.06.10

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Direct forces in a frame due to concentrated tangential loads.
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ESDU STRUCT 03.06.08 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Moments in a frame due to concentrated radial loads.

ESDU STRUCT 03.06.08

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Moments in a frame due to concentrated radial loads.
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ESDU STRUCT 03.06.06 1952 Edition, October 1, 1952
Flexible circular frames supported by a shell. Moments in a frame due to concentrated couples.

ESDU STRUCT 03.06.06

1952 Edition, October 1, 1952

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Flexible circular frames supported by a shell. Moments in a frame due to concentrated couples.
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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 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

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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

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Form factors for angle, tee and channel sections under combined bending and axial load.
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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

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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

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Information on the use of data sheets 01.06.
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ESDU STRUCT 02.04.06 1957 Edition, May 1, 1957
Initial buckling of flat isosceles triangular plates under combined compression and shear.

ESDU STRUCT 02.04.06

1957 Edition, May 1, 1957

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Initial buckling of flat isosceles triangular plates under combined compression and shear.
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ESDU STRUCT 02.01.46 1957 Edition, June 1, 1957
Buckling stress coefficients for flat parallelogram plates under uniform compression. (All edges fixed against rotation.)

ESDU STRUCT 02.01.46

1957 Edition, June 1, 1957

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Buckling stress coefficients for flat parallelogram plates under uniform compression. (All edges fixed against rotation.)
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ESDU STRUCT 01.01.23 1962 Edition, February 1, 1962
The buckling of a composite strut.

ESDU STRUCT 01.01.23

1962 Edition, February 1, 1962

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The buckling of a composite strut.
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ESDU STRUCT 03.06.16 1962 Edition, October 1, 1962
Flexible circular frames supporting a shell. Shear flow from shell to frame due to concentrated loads and couples.

ESDU STRUCT 03.06.16

1962 Edition, October 1, 1962

Complete Document
 
Flexible circular frames supporting a shell. Shear flow from shell to frame due to concentrated loads and couples.
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