The Aeronautical Quarterly, Volume 22 - November 1971
- This volume was published under a former title. See this journal's title history.
Research Article
Stagnation Pressure Changes in Unsteady Flow
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- 07 June 2016, pp. 207-224
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Laminar Compressible Boundary Layers with Non-Uniform Wall Temperatures
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- 07 June 2016, pp. 1-11
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Turbulent Jets and Wall Jets in Uniform Streaming Flow
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- 07 June 2016, pp. 311-326
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Wake Induced Flutter of Circular Cylinders: Mechanical Aspects
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- 07 June 2016, pp. 101-118
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Heat Transfer to Slender Bodies at a Mach Number of 5.2
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- 07 June 2016, pp. 12-24
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The Hypersonic Source Flow Past Wedges and Cones
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- 07 June 2016, pp. 327-345
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Experimental Results for Waveriders in Certain Off-Design Conditions
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- 07 June 2016, pp. 225-232
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Experimental Study of the Thermal Wake Interference Between Closely Spaced Wires of a X-Type Hot-Wire Probe
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- 07 June 2016, pp. 119-126
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On the Flutter of a Smooth Circular Cylinder in a Wake
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- 07 June 2016, pp. 25-41
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Numerical Calculations of the Hypersonic Viscid–Inviscid Flow Inside Simple Ducts of Circular Cross-Section
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- 07 June 2016, pp. 233-256
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Stability Derivatives of Sharp Wedges in Viscous Hypersonic Flow
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- 07 June 2016, pp. 127-145
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The Three-Dimensional Turbulent Boundary Layer on an Infinite Yawed Wing
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- 07 June 2016, pp. 346-362
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The Local Buckling and Post Local Buckling Behaviour of Thin-Walled Beams
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- 07 June 2016, pp. 363-388
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The Interaction of the Wake from an Oscillating Blade with a Fixed Cascade
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- 07 June 2016, pp. 42-52
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Vibration Characteristics of Pre-twisted Blades of Asymmetrical Aerofoil Cross-Section
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- 07 June 2016, pp. 257-273
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The Strongly Controlled Aircraft
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- 07 June 2016, pp. 146-168
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The Turbulent Boundary Layer on a Rotating Nose-Body
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- 07 June 2016, pp. 389-402
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The Prediction of Turbulent, Supersonic, Two-Dimensional, Boundary-Layer Flows
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- 07 June 2016, pp. 274-294
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Secondary Mass Injection in a Hypersonic Flow
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- 07 June 2016, pp. 53-64
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Eddy Viscosity Distributions in Compressible Turbulent Boundary Layers with Injection
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- 07 June 2016, pp. 169-182
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