Fifty Years of Flight Research
Fifty Years of Flight Research

Author: David F. Fisher

Publisher:

Published: 1999

Total Pages: 526

ISBN-13:

DOWNLOAD EBOOK

A bibliography of Technical Reports from Dryden Research Center, 1946-1996. Dryden was a National Advisory Committee for Aeronautics (NACA) facility from to 1946-1958, when NACA became NASA (National Aeronautics and Space Administration). This bibliography encompasses both NACA and NASA publications. Illustrated with diagrams and photos. Black and white version.

Aeronautical Engineering
Aeronautical Engineering

Author:

Publisher:

Published: 1973

Total Pages: 696

ISBN-13:

DOWNLOAD EBOOK

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Flight Dynamics Principles
Flight Dynamics Principles

Author: Michael V. Cook

Publisher: Butterworth-Heinemann

Published: 2012-10-03

Total Pages: 608

ISBN-13: 008098276X

DOWNLOAD EBOOK

The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. - Additional examples to illustrate the application of computational procedures using tools such as MATLAB®, MathCad® and Program CC® - Improved compatibility with, and more expansive coverage of the North American notational style - Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence - An additional coursework study on flight control design for an unmanned air vehicle (UAV)

Applied Nonlinear Control
Applied Nonlinear Control

Author: Jean-Jacques E. Slotine

Publisher:

Published: 1991

Total Pages: 461

ISBN-13: 9780130400499

DOWNLOAD EBOOK

In this work, the authors present a global perspective on the methods available for analysis and design of non-linear control systems and detail specific applications. They provide a tutorial exposition of the major non-linear systems analysis techniques followed by a discussion of available non-linear design methods.

Full-scale Wind-tunnel Tests of a Small Unpowered Jet Aircraft with a T-Tail
Full-scale Wind-tunnel Tests of a Small Unpowered Jet Aircraft with a T-Tail

Author: Paul T. Soderman

Publisher:

Published: 1971

Total Pages: 108

ISBN-13:

DOWNLOAD EBOOK

The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail were investigated in a 40 x 80 ft (12.2 by 24.4 meter) wind tunnel (subsonic). Static, longitudinal, and lateral stability, and control characteristics were determined at angles of attack from -2 deg to 42 deg. The aircraft wing had 13 deg of sweep and an aspect ratio of 5.02. The aircraft was tested power off with various wing leading- and trailing-edge high lift devices. The basic configuration was tested with and without such components as engine nacelles, wing tip tanks, and empannage. Hinge-moment data were obtained and downwash angles in the horizontal-tail plane location were calculated. The data were obtained at Reynolds numbers of 4.1 million and 8.7 million based on mean aerodynamic chord. The model had static longitudinal stability through initial stall. Severe tail buffet occurred near the angle of attack for maximum lift. Above initial stall the aircraft had pronounced pitch-up, characteristic of T-tail configurations. A stable trim point was possible at angles of attack between 30 deg and 40 deg (depending on c.g. location and flap setting). Hinge-moment data showed no regions with adverse effects on stick force. Comparisons of wind-tunnel data and flight-test are presented.