June 18, 2021

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General Aviation Aircraft Design

General Aviation Aircraft Design
Author : Snorri Gudmundsson
Publisher : Butterworth-Heinemann
Release Date : 2021-09-15
Category : Business & Economics
Total pages :1200
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It is imperative that the mission of a new aircraft is very clearly defined. Is it primarily intended to serve as a cruiser? If so, what airspeed and cruising altitude is it most likely to see during its operation? Is it a cargo transport aircraft? How much weight must it carry? How fast, far, and high shall it fly? General Aviation Aircraft Design: Applied Methods and Procedures, Second Edition continues to be the engineers' best source for answers to realistic aircraft design questions. The book provides design guidance for additional general aviation aircraft such as seaplanes, canards, UAV, and supersonic business aircraft. It also provides important tools and examples for aircraft sizing and design for good handling characteristics, and includes new chapters on: Thrust Modeling for Turbojet and Turbofan Engines Longitudinal Stability and Control Lateral Stability and Control Directional Stability and Control Dynamic Stability and Control Written by an engineer with over 20 years of design experience, professional engineers, aircraft designers, aerodynamicists, structural analysts, performance analysts, researchers, and advanced aerospace engineering students will value this book as the classic go-to for aircraft design. NEW: The printed book is in color! NEW: Design formulation for electric aircraft! More material, that includes three new chapters and two appendices Every chapter has been revised for more concise presentation 1011 Figures, illustrations, and graphs. Multiple new illustrations. Previous illustrations revised Discusses the most frequently used methods in conceptual aircraft design Covers various handling and stability topics such as roll, yaw, pitch competing control authority especially at low speeds, and the effects of uncommanded thrust/pitch reversal on control Features updated material to all the chapters including new sections to chapter 4 (Aircraft Conceptual Layout) and chapter 7 (Selecting the Power Plant), the addition of chapters on stability and control directed squarely at GA aircraft design and sizing, as well as regulations updated to "new" 14 CFR Part 23 Uses real-world examples and actual aircraft designs such as the Cirrus SR-22, solved examples, and derivations

General Aviation Aircraft Design

General Aviation Aircraft Design
Author : Snorri Gudmundsson
Publisher : Unknown
Release Date : 2013
Category : Engineering
Total pages :1048
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Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design. Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need Numerical examples involve actual aircraft specs Contains high-interest topics not found in other texts, including sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design Provides a unique safety-oriented design checklist based on industry experience Discusses advantages and disadvantages of using computational tools during the design process Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only).

General Aviation Aircraft Load Analysis

General Aviation Aircraft Load Analysis
Author : Snorri Gudmundsson
Publisher : Butterworth-Heinemann
Release Date : 2017-11-01
Category :
Total pages :416
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Load analysis is an indispensable preliminary element of aircraft structural design, defining aerodynamic, inertial, and operational loads that the airframe must be equipped to react to. Snorri Gudmundsson (author of General Aviation Aircraft Design) sets out to provide a clear and practical study of load analysis for general aviation aircraft-the first book on the market to do so. From explaining basic concepts like aerodynamic and inertial loads to covering new practical methods for calculation (including numerical and experimental analyses), General Aviation Load Analysis brings a level of detail benefiting those studying and working in general aviation aircraft structural design. The only book on the market that focuses exclusively on load for GA aircraft Balances basic concepts of load estimation and practical methods of load calculation Addresses load estimation using both numerical and experimental methods

Synthesis of Subsonic Airplane Design

Synthesis of Subsonic Airplane Design
Author : E. Torenbeek
Publisher : Springer Science & Business Media
Release Date : 2013-06-29
Category : Technology & Engineering
Total pages :598
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Since the education of aeronautical engineers at Delft University of Technology started in 1940 under tae inspiring leadership of Professor H.J. van der Maas, much emphasis has been placed on the design of aircraft as part of the student's curriculum. Not only is aircraft design an optional subject for thesis work, but every aeronautical student has to carry out a preliminary airplane design in the course of his study. The main purpose of this preliminary design work is to enable the student to synthesize the knowledge ob tained separately in courses on aerodynamics, aircraft performances, stability and con trol, aircraft structures, etc. The student's exercises in preliminary design have been directed through the years by a number of staff members of the Department of Aerospace Engineering in Delft. The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years. Not only has he acquired vast experience in teaching airplane design at university level, but he has also been deeply involved in design-oriented re search, e.g. developing rational design methods and systematizing design information. I am very pleased that this wealth of experience, methods and data is now presented in this book.

General Aviation Aircraft Design Methodology in a PC Environment

General Aviation Aircraft Design Methodology in a PC Environment
Author : Jan Roskram
Publisher : Unknown
Release Date : 1996
Category :
Total pages :129
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General Aviation Technology Conference

General Aviation Technology Conference
Author : Anonim
Publisher : Unknown
Release Date : 1964
Category : Electronic book
Total pages :129
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General Aviation Aircraft Design for Performance Using Small Computers

General Aviation Aircraft Design for Performance Using Small Computers
Author : Society of Automotive Engineers, Inc,J. C. Narramore
Publisher : Unknown
Release Date : 1979
Category :
Total pages :129
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General Aviation Aircraft Design

General Aviation Aircraft Design
Author : Snorri Gudmundsson
Publisher : Butterworth-Heinemann
Release Date : 2013-09-03
Category : Technology & Engineering
Total pages :1048
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Find the right answer the first time with this useful handbook of preliminary aircraft design. Written by an engineer with close to 20 years of design experience, General Aviation Aircraft Design: Applied Methods and Procedures provides the practicing engineer with a versatile handbook that serves as the first source for finding answers to realistic aircraft design questions. The book is structured in an "equation/derivation/solved example" format for easy access to content. Readers will find it a valuable guide to topics such as sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design. In most cases, numerical examples involve actual aircraft specs. Concepts are visually depicted by a number of useful black-and-white figures, photos, and graphs (with full-color images included in the eBook only). Broad and deep in coverage, it is intended for practicing engineers, aerospace engineering students, mathematically astute amateur aircraft designers, and anyone interested in aircraft design. Organized by articles and structured in an "equation/derivation/solved example" format for easy access to the content you need Numerical examples involve actual aircraft specs Contains high-interest topics not found in other texts, including sizing of horizontal and vertical tails to minimize drag, sizing of lifting surfaces to ensure proper dynamic stability, numerical performance methods, and common faults and fixes in aircraft design Provides a unique safety-oriented design checklist based on industry experience Discusses advantages and disadvantages of using computational tools during the design process Features detailed summaries of design options detailing the pros and cons of each aerodynamic solution Includes three case studies showing applications to business jets, general aviation aircraft, and UAVs Numerous high-quality graphics clearly illustrate the book's concepts (note: images are full-color in eBook only)

SEPARATE PAPERS PRESENTED AT THE AIAA GENERAL AVIATION AIRCRAFT DESIGN AND OPERATIONS MEETING.

SEPARATE PAPERS PRESENTED AT THE AIAA GENERAL AVIATION AIRCRAFT DESIGN AND OPERATIONS MEETING.
Author : Anonim
Publisher : Unknown
Release Date : 2021
Category :
Total pages :129
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Assessment of New Technologies for General Aviation Aircraft

Assessment of New Technologies for General Aviation Aircraft
Author : Anonim
Publisher : Unknown
Release Date : 1978
Category : Airplanes
Total pages :75
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This report assesses the use of new technologies in general aviation aircraft. It also investigates the potential for a technology demonstration program aimed specifically at the needs of general aviation. It concludes that at least 46 new or under-used technologies could be incorporated in general aviation aircraft with benefit to safety, performance and cost. The rate at which these new technologies might be integrated into the fleet will depend on social and political trends as well as on the technologies themselves. This report identifies 22 trends that will influence general aviation development. On the basis of the study results it appears that joint demonstration programs involving the FAA, NASA and industry would be valuable in introducing new technologies into general aviation aircraft design. (Author).

AIAA General Aviation Aircraft Design and Operation Meeting

AIAA General Aviation Aircraft Design and Operation Meeting
Author : Anonim
Publisher : Unknown
Release Date : 1964
Category :
Total pages :129
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Synthesis of Subsonic Airplane Design

Synthesis of Subsonic Airplane Design
Author : E. Torenbeek
Publisher : Unknown
Release Date : 2014-01-15
Category :
Total pages :624
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Preliminary Design Studies of an Advanced General Aviation Aircraft

Preliminary Design Studies of an Advanced General Aviation Aircraft
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Release Date : 2018-07-27
Category :
Total pages :204
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The preliminary design results are presented of the advanced aircraft design project. The goal was to take a revolutionary look into the design of a general aviation aircraft. Phase 1 of the project included the preliminary design of two configurations, a pusher, and a tractor. Phase 2 included the selection of only one configuration for further study. The pusher configuration was selected on the basis of performance characteristics, cabin noise, natural laminar flow, and system layouts. The design was then iterated to achieve higher levels of performance. Barrett, Ron and Demoss, Shane and Dirkzwager, AB and Evans, Darryl and Gomer, Charles and Keiter, Jerry and Knipp, Darren and Seier, Glen and Smith, Steve and Wenninger, ED Unspecified Center NASA-CR-190024, NAS 1.26:190024 NASW-4435...

The Balsa Bullet: A High Speed, Low-Cost General Aviation Aircraft for Aeroworld

The Balsa Bullet: A High Speed, Low-Cost General Aviation Aircraft for Aeroworld
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Release Date : 2018-11-23
Category : Science
Total pages :174
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The Balsa Bullet is a high speed, low cost six passenger general aviation aircraft. It will cruise at a speed of 55 ft/s with a maximum speed of 75 ft/s for distances in excess of 27000 feet. This range and speed combination provide The Balsa Bullet with the capability to service any two existing airports in Aeroworld in an efficient and timely manner. Overall, three major design drivers have been identified by the design team. The first is to provide a low cost airplane to the Aeroworld market. Maintaining the low cost objective will not simply meet the mission objective, but will also make the Bullet an economically viable option for a wide number of consumers. The Balsa Bullet has a total manufacturing cost of $1000 with a price to the consumer of only $2562. The second major driver is high speed performance. Once again this driver exists not only to meet the mission objective given Long Shot Aeronautics but it provides a desirable feature to the consumer, pride in owning the fastest aircraft in Aeroworld. The third design driver identified is the capability to service any runway in Aeroworld necessitating the ability to takeoff within 28 ft, the length of the shortest runways in Aeroworld. These design drivers provide three great reasons for the general public to purchase a Bullet. Eastland, Kevin and Greenwood, Sean and Kelly, Dan and Leonard, Chuck and Rooff, John and Scherock, Jeff AERODYNAMIC CHARACTERISTICS; AIRCRAFT DESIGN; AIRPORTS; BALSA; GENERAL AVIATION AIRCRAFT; HIGH SPEED; LIFT DRAG RATIO; LOW COST; PASSENGER AIRCRAFT; RUNWAYS; TAKEOFF; AIRCRAFT PERFORMANCE; AIRCRAFT PRODUCTION; DESIGN TO COST; SINGLE ENGINE AIRCRAFT; STUDENTS...

Icarus Rewaxed

Icarus Rewaxed
Author : National Aeronautics and Space Adm Nasa
Publisher : Unknown
Release Date : 2018-11-21
Category :
Total pages :170
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Icarus Rewaxed is a single engine, six passenger, general aviation airplane. With a cruise velocity of 72 ft/s, the Icarus can compete with the performance of any other airplane in its class with an eye on economics and safety. It has a very competitive initial price ($3498.00) and cost per flight ($6.36-8.40). Icarus can serve all airports in Aeroworld with a takeoff distance of 25.4 feet and maximum range of 38,000 feet. It is capable of taking off from an unprepared field with a grass depth of 3 inches. Icarus Rewaxed fills the market need for a high-speed, low cost aircraft. It provides customers with a general aviation craft that can compete in the existing performance market with the added security of an advanced structure. With the use of advanced materials, the maneuvering capability of the Icarus is increased, as it can withstand greater load factors than previous aircraft. Farrens, Bryan and Hueckel, Macy and Fulkerson, Dan and Barents, Matt and Capozzi, Brian and Ramsey, Keri AIRCRAFT DESIGN; AIRCRAFT MODELS; GENERAL AVIATION AIRCRAFT; MONOPLANES; PASSENGER AIRCRAFT; AERODYNAMICS; AIRCRAFT PERFORMANCE; HIGH SPEED; LOW COST; STRUCTURAL DESIGN...