CoA. Reports: Recent submissions

Now showing items 181-200 of 280

Eurilia (European Initiative in Library & Information in Aerospace) :

Blagden, J F
Eurilia (European Initiative in Library & Information in Aerospace) :

Harrington, John
On minimizing maximum transient energy growth

Whidborne, James F.; McKernan, John; Steer, Anthony J.
An empirical method for rapidly estimating the loading distributions on swept back wings

Stanton Jones, R. (Cranfield College of Aeronautics, )
Further tests of a laminar flow swept wing with boundary layer control by suction

Landeryou, R. R.; Porter, P. G. (Cranfield University, College of Aeronautics, )
Numerical computation of two-dimensional unsteady detonation waves in high energy solids

Clarke, J. F.; Karni, S.; Quirk, J. J.
Target position and trajectory measurements by videogrammetry

Hobbs, Stephen
Linear mixture modelling solution methods for satellite remote sensing

Hobbs, Stephen
Review of Initial Experiments Using the Hawk Model, Dynamic Rig Facility and the CED1401 Digital Data Acquisition Equipment : Seventh Quarterly Report

Hinds, H. A.; Cook, M. V. (Cranfield Institute of Technology; College of Aeronautics, )
Compressible Flow Produced by Distributed Sources of Mass: An Exact Solution

Clarke, J. F. (Aerodynamics, Cranfield Institute of Technology, )
The Linearised small perturbation equations of motion for an airship

Cook, M. V.
Formulation and System Identification of the Equations of Motion for a Dynamic Wind Tunnel Facility.

Carnduff, S. D.; Cooke, A. K. (Cranfield University, )
Debris removal from low earth orbit (DR LEO)

Hobbs, Stephen (Cranfield University, )
Flight test of a laminar flow swept wing with boundary layer control by suction

Landeryou, R. R.; Trayford, R. S.
Optimum design of a vortex tube for achieving large temperature drop ratios

Westley, R. (College of Aeronautics, Cranfield, )
The flow over delta wings at low speeds with leading edge separation

Marsden, D. J.; Simpson, R. W.; Rainbird, W. J. (College of Aeronautics, )
Optimum Mitchell Frameworks for Three Parallel Forces

Chan, H. S. Y. (Cranfield College of Aeronautics, )
The Design of Michell Optimum Structures

Chan, A. S. L. (Cranfield College of Aeronautics, )
On the use of approximate solutions for non linear oscillations

Padfield, Gareth D. (Cranfield College of Aeronautics, )
Euler calculations with emphasis on the nonoverlapped composite grid and hypersonic flows

Lin, Hong-Chia (Cranfield Institute of Technology; College of Aeronautics, )

Recently added

CoA. Reports: Recent submissions

Search AERADE

Browse

All of AERADE

This Collection

My Account