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Introduction to Aircraft Flight Mechanics: Performance, Static and Dynamic Stability, Classical Feedback Control, with State-Space and Rotorcraft Foundations

Description:

Introduction to Aircraft Flight Mechanics, Third Edition revises and expands this acclaimed, widely adopted textbook. Outstanding for use in undergraduate aeronautical engineering curricula, it is written for those first encountering the topic by clearly explaining the concepts and derivations of equations involved in aircraft flight mechanics. It begins with a review of basic aerodynamics and propulsion and continues through aircraft performance, equations of motion, static stability, linearizing equations of motion, dynamic stability, classical feedback control, stability and control augmentation, Bode, state space, and special topics. The third edition includes extensive updates to the first ten chapters and new chapters covering propeller theory and rotorcraft analysis. Chapter 13 provides interesting design insights on the A-10 Close Air Support aircraft. Past winner of the AIAA Summerfield Book Award, this text contributes greatly to learning the fundamental principles of flight mechanics that are a crucial foundation of any aeronautical engineering curricula. It contains both real-world applications and problems. Across the first, second, and now third editions, actual field experience from the engineering and fl ying communities along with constructive feedback from several university professors has been incorporated.


Editorial Reviews

About the Author

TOM YECHOUT is a Professor of Aeronautical Engineering at the U.S. Air Force Academy. He earned his Doctor of Engineering degree in Aerospace Engineering from the University of Kansas and is an AIAA Fellow. He is the recipient of numerous awards including the NASA Outstanding Achievement Award, Frank J. Seiler Award for Research Excellence, and the Heiser Award as the Outstanding USAFA Senior Faculty Educator. He was also honored by the Carnegie Foundation as the 2011 Colorado Professor of the Year. His background includes development and flight testing of the F/FB-111, A-7D, F-4E, and Lear 35 aircraft as well as extensive with the A-10. In addition, he has served as the principal investigator for numerous wind tunnel investigation programs, holds the patent for the Rakelet wing tip modification concept, and has authored over 200 technical publications.

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Introduction to Aircraft Flight Mechanics: Performance, Static and Dynamic Stability, Classical Feedback Control, with State-Space and Rotorcraft Foundations

Product ID: U1624107249
Condition: New

5

AED93271

Price includes VAT & Import Duties
Type: Hardcover
Availability: In Stock

Quantity:

|

Order today to get by 7-14 business days

This item qualifies for free delivery

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Imported From: United States

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Introduction to Aircraft Flight Mechanics: Performance, Static and Dynamic Stability, Classical Feedback Control, with State-Space and Rotorcraft Foundations

Product ID: U1624107249
Condition: New

5

Introduction to Aircraft Flight Mechanics: Performance, Static and Dynamic Stability, Classical Feedback Control, with State-Space and Rotorcraft Foundations-0
Type: Hardcover

AED93271

Price includes VAT & Import Duties
Availability: In Stock

Quantity:

|

Order today to get by 7-14 business days

This item qualifies for free delivery

Returns & Warranty policies

Imported From: United States

At BOLO, we work hard to ensure the products you receive are new, genuine, and sourced from reputable suppliers.

BOLO is not an authorized or official retailer for most brands, nor are we affiliated with manufacturers unless specifically stated on a product page. Instead, we source verified sellers, authorized distributors or directly from the manufacturer.

Each product undergoes thorough inspection and verification at our consolidation and fulfilment centers to ensure it meets our strict authenticity and quality standards before being shipped and delivered to you.

If you ever have concerns regarding the authenticity of a product purchased from us, please contact Bolo Support. We will review your inquiry promptly and, if necessary, provide documentation verifying authenticity or offer a suitable resolution.

Your trust is our top priority, and we are committed to maintaining transparency and integrity in every transaction.

All product information, images, descriptions, and reviews originate from the manufacturer or from trusted sellers overseas. BOLO is not affiliated with, endorsed by, or an authorized retailer for most brands listed on our website unless stated otherwise.

While we strive to display accurate information, variations in packaging, labeling, instructions, or formulation may occasionally occur due to regional differences or supplier updates. For detailed or manufacturer-specific information, please contact the brand directly or reach out to BOLO Support for assistance.

Unless otherwise stated, all prices displayed on the product page include applicable taxes and import duties.

BOLO operates in accordance with the laws and regulations of United Arab Emirates. Any items found to be restricted or prohibited for sale within the UAE will be cancelled prior to shipment. We take proactive measures to ensure that only products permitted for sale in United Arab Emirates are listed on our website.

All items are shipped by air, and any products classified as “Dangerous Goods (DG)” under IATA regulations will be removed from the order and cancelled.

All orders are processed manually, and we make every effort to process them promptly once confirmed. Products cancelled due to the above reasons will be permanently removed from listings across the website.

Description:

Introduction to Aircraft Flight Mechanics, Third Edition revises and expands this acclaimed, widely adopted textbook. Outstanding for use in undergraduate aeronautical engineering curricula, it is written for those first encountering the topic by clearly explaining the concepts and derivations of equations involved in aircraft flight mechanics. It begins with a review of basic aerodynamics and propulsion and continues through aircraft performance, equations of motion, static stability, linearizing equations of motion, dynamic stability, classical feedback control, stability and control augmentation, Bode, state space, and special topics. The third edition includes extensive updates to the first ten chapters and new chapters covering propeller theory and rotorcraft analysis. Chapter 13 provides interesting design insights on the A-10 Close Air Support aircraft. Past winner of the AIAA Summerfield Book Award, this text contributes greatly to learning the fundamental principles of flight mechanics that are a crucial foundation of any aeronautical engineering curricula. It contains both real-world applications and problems. Across the first, second, and now third editions, actual field experience from the engineering and fl ying communities along with constructive feedback from several university professors has been incorporated.


Editorial Reviews

About the Author

TOM YECHOUT is a Professor of Aeronautical Engineering at the U.S. Air Force Academy. He earned his Doctor of Engineering degree in Aerospace Engineering from the University of Kansas and is an AIAA Fellow. He is the recipient of numerous awards including the NASA Outstanding Achievement Award, Frank J. Seiler Award for Research Excellence, and the Heiser Award as the Outstanding USAFA Senior Faculty Educator. He was also honored by the Carnegie Foundation as the 2011 Colorado Professor of the Year. His background includes development and flight testing of the F/FB-111, A-7D, F-4E, and Lear 35 aircraft as well as extensive with the A-10. In addition, he has served as the principal investigator for numerous wind tunnel investigation programs, holds the patent for the Rakelet wing tip modification concept, and has authored over 200 technical publications.

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