Preliminary note on the effect of inertia cross-coupling on aircraft response in rolling manoeuvres View on Open Library

Preliminary note on the effect of inertia cross-coupling on aircraft response in rolling manoeuvres

by W. J. G. Pinsker

No reviews yet
First published: 1959

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by W. J. G. Pinsker

The control characteristics of aircraft employing direct-lift control

The control characteristics of aircraft ...

Directional stability in flight with bank angle constraint as a condition defining a minimum acceptable value for n[superscript v]

Directional stability in flight with ban...

A form of lateral instability of lifting free-flight models towed by a helicopter

A form of lateral instability of lifting...

The landing flare of large transport aircraft

The landing flare of large transport air...

A semi-empirical method for estimating the rotary rolling moment derivatives of swept and slender wings

A semi-empirical method for estimating t...

The flight simulator in aircraft control and design

The flight simulator in aircraft control...