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Whirl Flutter of Turboprop Aircraft Structures

  • 2nd Edition - January 13, 2023
  • Latest edition
  • Author: Jiří Čečrdle
  • Language: English

Whirl Flutter of Turboprop Aircraft Structures, Second Edition explores the whirl flutter phenomenon, including theoretical, practical, analytical and experimental aspects o… Read more

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Description

Whirl Flutter of Turboprop Aircraft Structures, Second Edition explores the whirl flutter phenomenon, including theoretical, practical, analytical and experimental aspects of the matter. Sections provide a general overview regarding aeroelasticity, discussions on the physical principle and the occurrence of whirl flutter in aerospace practice, and experimental research conducted, especially from the 60s. Other chapters delve into analytical methods such as basic and advanced linear models, non-linear and CFD based methods, certification issues including regulation requirements, a description of possible certification approaches, and several examples of aircraft certification from aerospace.

Finally, a database of relevant books, reports and papers is provided. This updated and expanded second edition covers new chapters including both analytical and experimental aspects of the subject matter.

Key features

  • Provides complex information on turboprop aircraft whirl flutter phenomenon
  • Presents both theoretical and practical (certification related) issues
  • Includes experimental research as well as analytical models (basic and advanced) of matter
  • Includes both early-performed works and recent developments
  • Contains a listing of relevant books and reports

Readership

Aeroelasticity researchers in industrial and academic research institutes with an interest in turboprop aircraft.

Table of contents

1. Introduction to aircraft aeroelasticity and whirl flutter

1.1 Scope of aeroelasticity

1.2 Static aeroelastic phenomena

1.3 Dynamic aeroelastic phenomena

2. Theoretical background of the whirl flutter phenomenon

2.1 Physical principle

2.2 Propeller whirl flutter

2.3 Tilt-rotor whirl flutter
References

3. Whirl flutter occurrence in aerospace practice

3.1 Introduction

3.2 Lockheed L-188C Electra II

3.3 Beechcraft 1900C

3.4 Other aircraft
References

4. Experimental research into whirl flutter

4.1 Introduction

4.2 Early tests (1930s)

4.3 Main developments (1960s)

4.4 Recent activities

4.5 W-WING whirl-flutter demonstrator
References

5. Analytical methods for whirl flutter investigation

5.1 Historical overview

5.2 Fundamental solution

5.3 Influences of major parameters

5.4 Propeller aerodynamic forces by strip theory

5.5 Lift lag effect

5.6 Blade lift curve slope and Mach number effects

5.7 Correction to number of propeller blades

5.8 Influence of wing flexibility

5.9 Influence of hinged blade flexibility

5.10 Influence of gimbaled propeller flexibility

5.11 Influence of twisted blade flexibility

5.12 Propeller aerodynamic forces by lifting surface theory

5.13 Model of coupled bending blades

5.14 Complex models for tilt-rotor applications

5.15 Rear fuselage-mounted engines

5.16 Two-bladed propellers
References

6. Application to the aircraft certification process

6.1 Requirements of the airworthiness regulations

6.2 Analytical approaches
References

7. Certification examples from aerospace practice

7.1 Single nose-mounted engine utility aircraft

7.2 Twin wing-mounted engine utility aircraft

7.3 Twin wing-mounted engine commuter aircraft with tip-tanks
References

Nomenclature
Index

Product details

  • Edition: 2
  • Latest edition
  • Published: January 13, 2023
  • Language: English

About the author

Jiří Čečrdle

Jiří Čečrdle started his professional carrier in 1995 at the Czech Aerospace Research Centre (VZLU) in Prague, Czech Republic. He has been the head of the Workgroup of Aeroelasticity there since 2004. He participated in several projects of Czech aircraft development and certification, and he also works as a Compliance Verification Engineer (CVE) and research project evaluator. His spheres of scientific interest include analytical and experimental dynamics and the aeroelasticity of aircraft structures, as well as aeroelastic optimization and model updating. His whirl flutter-related experience includes aircraft certification issues, the development of analytical tools and methods and the development of the whirl flutter aeroelastic wind tunnel demonstrator.
Affiliations and expertise
Senior Scientist, Czech Aerospace Research Centre (VZLU), Prague, Czech Republic.

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