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Image for Wave Drag of Flat Plates with Blunt Noses at Zero Incidence

Wave Drag of Flat Plates with Blunt Noses at Zero Incidence

series Aerodynamics
Loose-leaf 1 Aug 1964
ISBN: 9781862464636
Dewey: 533.62
£150.00
Image for Base Pressure on Aerofoil Sections with a Blunt Trailing Edge in Supersonic Flow

Base Pressure on Aerofoil Sections with a Blunt Trailing Edge in Supersonic Flow

series Aerodynamics
Loose-leaf 1 Apr 1954
ISBN: 9781862464612
Dewey: 629.132305
£150.00
Image for Flexible Circular Frames Supported by a Shell : Direct Forces in a Frame Due to Concentrated Tangential Loads

Flexible Circular Frames Supported by a Shell : Direct Forces in a Frame Due to Concentrated Tangential Loads

series Aircraft Structures
Loose-leaf 1 Oct 1952
ISBN: 9781862465589
Dewey: 624.1773
£150.00
Image for Limit of Grain Size for Laminar Flow Over Wings or Bodies

Limit of Grain Size for Laminar Flow Over Wings or Bodies

series Aerodynamics
Loose-leaf 1 Apr 1953
ISBN: 9781862464537
Dewey: 533.215
£150.00
Image for Introductory Item on Two-dimensional Aerofoils at Supersonic Speeds : Amendment A

Introductory Item on Two-dimensional Aerofoils at Supersonic Speeds : Amendment A

series Aerodynamics
Loose-leaf 1 Apr 1956
ISBN: 9781862464568
Dewey: 629.132305
£150.00
Image for Initial Buckling of Slightly Curved Plates Under Combined Longitudinal and Circumferential Direct Stress (All Edges Simply-supported)

Initial Buckling of Slightly Curved Plates Under Combined Longitudinal and Circumferential Direct Stress (All Edges Simply-supported)

series Engineering Structures S.
Loose-leaf 1 Dec 1964
ISBN: 9781862465374
Dewey: 620.112
£150.00
Image for Flexible Circular Frames Supported by a Shell : Shear Forces in a Frame Due to Conentrated Radial Loads

Flexible Circular Frames Supported by a Shell : Shear Forces in a Frame Due to Conentrated Radial Loads

series Aircraft Structures
Loose-leaf 1 Oct 1952
ISBN: 9781862465626
Dewey: 624.1773
£150.00
Image for The Effect of Mean Stress on Fatigue Strength (Test Piece with Stress Concentration) (Fat A.00.02) : Amendment A

The Effect of Mean Stress on Fatigue Strength (Test Piece with Stress Concentration) (Fat A.00.02) : Amendment A

series Fatigue: Endurance Data S.
Loose-leaf 1 Jun 1958
ISBN: 9781862464698
Dewey: 620.112
£150.00
Image for Average and Edge Stresses for Thin Flat Aluminium Alloy Plates in Compression : Amendment A

Average and Edge Stresses for Thin Flat Aluminium Alloy Plates in Compression : Amendment A

series Aircraft Structures
Loose-leaf 1 Dec 1947
ISBN: 9781862465183
Dewey: 620.112
£150.00
Image for Information on the Use of Data Sheets 01.06.

Information on the Use of Data Sheets 01.06.

series Aircraft Structures
Loose-leaf 1 Nov 1956
ISBN: 9781862465121
Dewey: 624.17
£75.00
Image for Endurance of Bonded Double Strap Joints (Aluminium Alloy Sheet Material; Phenolic Resin/vinyl Powder Glue, Tensile Loading) (Fat E.05.07) : Amendment A

Endurance of Bonded Double Strap Joints (Aluminium Alloy Sheet Material; Phenolic Resin/vinyl Powder Glue, Tensile Loading) (Fat E.05.07) : Amendment A

series Fatigue: Endurance Data S.
Loose-leaf 1 May 1964
ISBN: 9781862464735
Dewey: 620.112
£150.00
Image for Performance Reduction for Aircraft with Turbo-props

Performance Reduction for Aircraft with Turbo-props

series Performance of Aircraft
Loose-leaf 1 Jul 1948
ISBN: 9781862464964
Dewey: 629.133343
£150.00
Image for Endurance of Bonded Lap Joints (Aluminium Alloy Sheet Material; Phenolic Resin/vinyl Powder Glue, Tensile Loading) (Fat E.05.06)

Endurance of Bonded Lap Joints (Aluminium Alloy Sheet Material; Phenolic Resin/vinyl Powder Glue, Tensile Loading) (Fat E.05.06)

series Fatigue: Endurance Data S.
Loose-leaf 1 May 1964
ISBN: 9781862464728
Dewey: 620.112
£150.00
Image for Flexible Circular Frames Supporting a Shell : Displacements Due to Concentrated Loads and Couples : Amendment A

Flexible Circular Frames Supporting a Shell : Displacements Due to Concentrated Loads and Couples : Amendment A

series Aircraft Structures
Loose-leaf 1 Aug 1964
ISBN: 9781862465633
Dewey: 624.1773
£150.00
Image for Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Skin with Integral Unflanged Stiffeners : Amendment B

Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Skin with Integral Unflanged Stiffeners : Amendment B

series Aircraft Structures
Loose-leaf 1 Jun 1954
ISBN: 9781862465299
Dewey: 620.11242
£150.00
Image for Drag of a Smooth Flat Plate at Zero Incidence : Amendment B

Drag of a Smooth Flat Plate at Zero Incidence : Amendment B

series Aerodynamics
Loose-leaf 1 Jul 1947
ISBN: 9781862464506
Dewey: 533.62
£150.00
Image for Flexible Circular Frames Supported by a Shell. Moments in a Frame Due to Concentrated Couples

Flexible Circular Frames Supported by a Shell. Moments in a Frame Due to Concentrated Couples

series Aircraft Structures
Loose-leaf 1 Oct 1952
ISBN: 9781862465541
Dewey: 624.1773
£150.00
Image for Flexible Circular Frames Supported by a Shell : Direct Forces in a Frame Due to Concentrated Radial Loads

Flexible Circular Frames Supported by a Shell : Direct Forces in a Frame Due to Concentrated Radial Loads

series Aircraft Structures
Loose-leaf 1 Oct 1952
ISBN: 9781862465596
Dewey: 624.1773
£150.00
Image for Buckling Stress Coefficients for Flat Plates Tapered in Plan, Under Compression

Buckling Stress Coefficients for Flat Plates Tapered in Plan, Under Compression

series Aircraft Structures
Loose-leaf 1 Jul 1963
ISBN: 9781862465350
Dewey: 620.11242
£150.00
Image for Average and Edge Stresses for Flat Plates Under Shear and Compression : Amendment A

Average and Edge Stresses for Flat Plates Under Shear and Compression : Amendment A

series Engineering Structures S.
Loose-leaf 1 Jan 1944
ISBN: 9781862465435
Dewey: 620.11242
£150.00
Image for Method of Calculating Stress Distribution in a Reinforced Symmetrical Shell Under Bending : Amendment A

Method of Calculating Stress Distribution in a Reinforced Symmetrical Shell Under Bending : Amendment A

series Aircraft Structures
Loose-leaf 1 Jan 1944
ISBN: 9781862465008
Dewey: 624.17762
£150.00
Image for Analytical Method of Performance Reduction for Aircraft with Turbo-jets : Rate of Climb

Analytical Method of Performance Reduction for Aircraft with Turbo-jets : Rate of Climb

series Performance of Aircraft
Loose-leaf 1 Jul 1948
ISBN: 9781862464872
Dewey: 629.1345
£150.00
Image for Radial Deflections of Circular Frame Due to Concentrated Loads and Couples : Amendment A

Radial Deflections of Circular Frame Due to Concentrated Loads and Couples : Amendment A

series Aircraft Structures
Loose-leaf 1 Nov 1944
ISBN: 9781862465527
Dewey: 624.172
£150.00
Image for Form Factors for Flanged Sections Under Combined Bending and Axial Load

Form Factors for Flanged Sections Under Combined Bending and Axial Load

series Aircraft Structures
Loose-leaf 1 Oct 1956
ISBN: 9781862465145
Dewey: 620.112
£150.00
Image for Standard British Method of Performance Reduction for Piston-engined Aircraft with Constant-speed Propellers : Fuel Consumption

Standard British Method of Performance Reduction for Piston-engined Aircraft with Constant-speed Propellers : Fuel Consumption

series Performance of Aircraft
Loose-leaf 1 Oct 1950
ISBN: 9781862464919
Dewey: 629.133343
£150.00
Image for The Strength of Struts : Amendment C

The Strength of Struts : Amendment C

series Aircraft Structures
Loose-leaf 1 Nov 1983
ISBN: 9781862465077
Dewey: 620.112
£150.00
Image for Buckling Stress Coefficients for Curved Plate Sin Shear Circumferential Length Exceeding Axial Length, Edges Simply-supported

Buckling Stress Coefficients for Curved Plate Sin Shear Circumferential Length Exceeding Axial Length, Edges Simply-supported

series Aircraft Structures
Loose-leaf 1 Oct 1952
ISBN: 9781862465404
Dewey: 620.112
£150.00
Image for Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Corrugated Sandwich Panel : Amendment B

Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Corrugated Sandwich Panel : Amendment B

series Aircraft Structures
Loose-leaf 1 Jun 1954
ISBN: 9781862465329
Dewey: 620.11242
£150.00
Image for Moments in Circular Frame Due to Conentrated Loads and Couples : Amendment A

Moments in Circular Frame Due to Conentrated Loads and Couples : Amendment A

series Aircraft Structures
Loose-leaf 1 Nov 1944
ISBN: 9781862465497
Dewey: 624.172
£150.00
Image for Estimation of Rolling Manoeuvrability

Estimation of Rolling Manoeuvrability

series Performance of Aircraft
Loose-leaf 1 Mar 1959
ISBN: 9781862464834
Dewey: 629.1345
£150.00
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