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stepwise regression

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View Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk By H. A. Hinds

Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk

Measurement of the longitudinal static stability and the moments of 0inertia of a 1/12th scale model of a B.Ae Hawk

By H. A. Hinds

View Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters By M. V. Cook

Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters

Initial review of research into the application of modified stepwise regression for the estimation of aircraft stability and control parameters

By M. V. Cook

View Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment By H. A. Hinds

Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment

Review of initial experiments using the Hawk model, dynamic rig facility and the CED1401 digital data acquisition equipment

By H. A. Hinds

View Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters By H. A. Hinds

Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters

Third quarterly report on the application of modified stepwise regression for the estimation of aircraft stability and control parameters

By H. A. Hinds

View Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data By J. C. Hoff

Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data

Initial evaluation of the modified stepwise regression procedure to estimate aircraft stability and control parameters from flight test data

By J. C. Hoff