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Now showing items 281-300 of 3498

Motion of a rigid body in an unsteady non-uniform heavy fluid :

Thomasson, P. G.
Fully discrete arbitrary-order schemes for a model hyperbolic conservation law

Shi, Jian; Toro, E. F.
Multi-dimensional WAF-type schemes for model conservation laws

Toro, E. F.
Comparison of the time vector method and the state-space method (Eigenvector analysis) for aircraft parameter identification

Baek, Y.
GENENG : A generic turboprop engine model

Pant, Rajkumar S.
Control jet-slender body performance characteristics at hypersonic speeds

Kontis, Konstantinos
Riemann solvers for solving the incompressible Navier-Stokes equations using the artificial compressibility method

Elsworth, D. T.; Toro, E. F.
Aircraft parameter identification using Matlab

Unknown author
Descriptions of Cranfield Aircraft Group design projects (1979-96)

Fielding, J. P.
The stability and control characteristics of the neutrally bouyant non-rigid airship

Goineau, F.
Fully discrete high-order schemes for hyperbolic conservation law.

Shi, Jian
An investigation into the potential use of psychometric instruments for the selection of firearms officers

Gleave, Susan
Structural impact simulation using program Krash

Liaw, J. C.
Motion of a rigid body in an unsteady non-uniform heavy fluid

Thomasson, P. G.
The applications of computational fluid dynamics to problems in rotorcraft aerodynamics:

Shaw, Scott
Flow studies at hypersonic speeds

Babinsky, Holger
The longitudinal controls fixed static stability of tailless aircraft

de Castro, Helena V.
Investigating the PIO-susceptibility of the F-4C

Brieger, Oliver
ASTOVL combat aircraft design synthesis and optimization

Kehayas, N.
A linearised Reimann solver for Gudonov-type methods

Toro, E. F.

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