Short University Courses

Guided Weapons Aerodynamics

Cranfield University, In Shrivenham
Length
5 days
Price
1,925 GBP excl. VAT
Next course start
Please enquire for course dates See details
Course delivery
Classroom
Length
5 days
Price
1,925 GBP excl. VAT
Next course start
Please enquire for course dates See details
Course delivery
Classroom
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Course description

A one-week introduction to propulsion and aerodynamic theory, specifically related to guided weapon systems.

Upcoming start dates

1 start date available

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  • Classroom
  • Shrivenham
  • English

Outcome / Qualification etc.

What you will learn

On successful completion of this module a student should be able to:

  • Apply the fundamental laws of fluid mechanics and aerodynamics to subsonic and supersonic missile systems;
  • Estimate the aerodynamic characteristics of typical missile systems, as needed for subsequent stability and control analysis;
  • Evaluate the trade-offs involved between missile aerodynamic design and other disciplines.

Training Course Content

Core content

  • Fundamental Definitions: Fluids, fluid properties, basic equations, ISA.
  • Basic Fluid Dynamics: Streamlines and streamtubes, continuity equation, Bernoulli’s equation, pressure coefficient, airspeed measurement, isentropic flow.
  • Hydrodynamics: Buoyancy, virtual mass effects, cavitation and ventilation.
  • Basic Aerodynamics: Viscous flow, Reynolds number, boundary layers, lift and drag, force and moment coefficients, wind tunnel testing.
  • Origins of Lift: Aerofoil section and wing geometry, physical theory, circulation theory, pressure distributions, lift curves, 3-D lift, centre of pressure, aerodynamic centre.
  • Subsonic Drag: Profile drag, downwash, induced drag, drag reduction, winglets.
  • Compressible Flow: Subsonic and supersonic propagation of disturbances, von Karman’s rules of supersonic flow, sound waves, flows around convex and concave corners, Prandtl-Mayer expansion fans.
  • Transonic Flow: Prandtl-Glauert theory, sound barrier problems, supercritical wing sections.
  • Supersonic Flow: Ackeret theory, supersonic wing sections, drag breakdown, unswept supersonic wings, Subsonic.
  • GW Aerodynamics Applications: Weapon aerodynamics, aerofoil sections, swept wing, slender delta wings, bodies (axial and normal force), wing/body combinations, controls, missile trim and stability, aerodynamic derivatives, aerodynamic interactions, high angle of attack aerodynamics, aerodynamic heating and heat transfer.
  • General Aerodynamics: Supporting tutorials.
  • Weapon Aerodynamics: Supporting tutorials.

Course delivery details

Course structure

Classroom lectures and tutorials. Virtual Learning Environment (VLE)-directed study.

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Cranfield University
College Road
MK43 0AL Cranfield

Cranfield University

Cranfield is a specialist postgraduate university that is a global leader for education and transformational research in technology and management. We have many world-class, large-scale facilities, including our own global research airport, which offers a unique environment for transformational education...

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