Buy Now, Pay Later
- – 4-month term
- – No impact on credit
- – Instant approval decision
- – Secure and straightforward checkout
Ready to go? Add this product to your cart and select a plan during checkout.
Payment plans are offered through our trusted finance partners Klarna, Affirm, Afterpay, Apple Pay, and PayTomorrow. No-credit-needed leasing options through Acima may also be available at checkout.
Learn more about financing & leasing here.
This item is eligible for return within 30 days of receipt
To qualify for a full refund, items must be returned in their original, unused condition. If an item is returned in a used, damaged, or materially different state, you may be granted a partial refund.
To initiate a return, please visit our Returns Center.
View our full returns policy here.
Description
Airplane Flight Dynamics & Automatic Flight Controls, Part I, provides exhaustive coverage of the methods for analysis and synthesis of the steady state and perturbed state (open loop) stability and control of fixed wing aircraft. This widely used book has been updated with modern flying quality criteria and aerodynamic data. Throughout this text, the practical (design) applications of the theory are stressed with many examples and illustrations. Aircraft stability and control characteristics are all heavily regulated by civil as well as by military airworthiness authorities for safety reasons. The role of the these safety regulations in the application of the theory is therefore stressed throughout. Airplane Flight Dynamics & Automatic Flight Controls, Part I is an essential reference for all aeronautical engineers working in the area of stability and control, regardless of experience levels. The book minimizes reader confusion through a systematic progression of fundamentals: - General steady and perturbed state equations of motion for a rigid airplane - Concepts and use of stability & control derivatives - Physical and mathematical explanations of stability & control derivatives - Solutions and applications of the steady state equations of motion from a viewpoint of airplane analysis and emphasis on airplane trim, take-off rotation and engine-out control - Open loop transfer functions - Analysis of fundamental dynamic modes: phugoid, short period, roll, spiral and dutch roll - Equivalent stability derivatives and the relation to automatic control of unstable airplanes - Flying qualities and the Cooper-Harper scale: civil and military regulations - Extensive numerical data on stability, control and hingemoment derivatives Read more
Publisher : Design, Analysis and Research Corporation (DARcorporation); 8th edition (September 26, 2018)
Publication date : September 26, 2018
Language : English
File size : 228329 KB
Text-to-Speech : Not enabled
Enhanced typesetting : Not Enabled
X-Ray : Not Enabled
Word Wise : Not Enabled
Format : Print Replica
Frequently asked questions
To initiate a return, please visit our Returns Center.
View our full returns policy here.
- Klarna Financing
- Affirm Pay in 4
- Affirm Financing
- Afterpay Financing
- PayTomorrow Financing
- Financing through Apple Pay
Learn more about financing & leasing here.
Similar Products
When Dark Winds Blow
The Gazebo
Say When