Coverart for item
The Resource Foundations of circulation control based small-scale unmanned aircraft : a comprehensive methodology from concept to design and experimental testing, Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford, (electronic resource)

Foundations of circulation control based small-scale unmanned aircraft : a comprehensive methodology from concept to design and experimental testing, Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford, (electronic resource)

Label
Foundations of circulation control based small-scale unmanned aircraft : a comprehensive methodology from concept to design and experimental testing
Title
Foundations of circulation control based small-scale unmanned aircraft
Title remainder
a comprehensive methodology from concept to design and experimental testing
Statement of responsibility
Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford
Creator
Contributor
Subject
Language
eng
Member of
http://library.link/vocab/creatorName
Kanistras, Konstantinos
Dewey number
  • 629.133/39
  • 620
Index
no index present
Literary form
non fiction
Nature of contents
dictionaries
http://library.link/vocab/relatedWorkOrContributorName
  • Valavanis, K.
  • Rutherford, Matthew J
Series statement
Intelligent Systems, Control and Automation: Science and Engineering
Series volume
v.91
http://library.link/vocab/subjectName
  • Drone aircraft
  • Drone aircraft
Label
Foundations of circulation control based small-scale unmanned aircraft : a comprehensive methodology from concept to design and experimental testing, Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford, (electronic resource)
Instantiates
Publication
Note
  • Description based upon print version of record
  • ""12 Epilogue""
Antecedent source
file reproduced from an electronic resource
Contents
  • ""Preface""; ""Acknowledgements""; ""Contents""; ""Acronyms""; ""1 Introduction""; ""1.1 Background Information""; ""1.2 Motivation""; ""1.3 Introduction to the Problem""; ""1.4 Method of Approach""; ""1.5 Outline of the Research Monograph""; ""2 Aircraft Performance and Design""; ""2.1 Design Considerations""; ""2.1.1 Wing Design""; ""2.1.2 Aircraft Tail Design""; ""2.2 Remarks""; ""3 Fundamentals of Circulation Control""; ""3.1 Vorticity and Circulation""; ""3.1.1 Kevin's and Helmholtz's Vortex Theorems""; ""3.1.2 Finite Wing Theory""; ""3.2 Coand Effect""; ""3.2.1 2-D Analysis""
  • ""3.2.2 Coand Jet Circulation Control""""3.3 Remarks""; ""4 The History of Circulation Control""; ""4.1 Numerical Analysis""; ""4.2 Experimental Work""; ""4.2.1 CC on Full-Scale Aircraft""; ""4.2.2 Circulation Control on Unmanned Aerial Vehicles""; ""4.3 Remarks""; ""5 Airfoil and Flap Design""; ""5.1 Coand Surfaces""; ""5.1.1 Airfoil Shapes""; ""5.1.2 Dual Radius Flap Geometry""; ""5.1.3 CCW Wind Tunnel Model""; ""5.2 Remarks""; ""6 Plenum Design""; ""6.1 Plenum Geometry""; ""6.1.1 Preliminary Plenum Design""; ""6.1.2 Diffuser-Based Plenum Design""; ""6.2 Remarks""; ""7 Instrumentation""
  • ""7.1 Wind Tunnel""""7.2 Force Balance""; ""7.2.1 The Concept""; ""7.2.2 Setup""; ""7.2.3 Calibration""; ""7.3 Pitot Probe""; ""7.4 Remarks""; ""8 Wind Tunnel Results and Discussion""; ""8.1 No Blowing and Blowing Case Comparison""; ""8.1.1 Effect of Blowing on Lift Coefficient CL""; ""8.1.2 Lift-to-Drag Ratio""; ""8.2 NACA 0015 CCW Configuration""; ""8.2.1 Wind Tunnel Test Conditions""; ""8.2.2 Cruise Flight Performance, 0o Flap Deflection""; ""8.2.3 High-Lift Takeoff Performance, 30o Flap Deflection""; ""8.2.4 High-Lift Takeoff Performance, 60o Flap Deflection""
  • ""8.2.5 Further Data Analysis""""8.3 Remarks""; ""9 UC2AV: Unmanned Circulation Control Aerial Vehicle""; ""9.1 The Aircraft""; ""9.2 Air Supply Unit and Air Delivery System""; ""9.2.1 Air Supply Unit""; ""9.2.2 Air Delivery System""; ""9.3 Circulation Control System""; ""9.4 Circulation Control Wing""; ""9.4.1 CCW Structural Analysis""; ""9.4.2 NACA 0015 Wing Implementation""; ""9.4.3 Circulation Control Wing Implementation""; ""9.5 Remarks""; ""10 Aircraft Takeoff Performance""; ""10.1 Takeoff Performance""; ""10.1.1 Takeoff Distance""; ""10.1.2 Pilot Takeoff Technique and Corrections""
  • ""10.1.3 One-at-a-Time Sensitivity Analysis""""10.2 Instrumentation and Sensors""; ""10.3 Remarks""; ""11 Flight Testing""; ""11.1 Aircraft Controls and Data Collection""; ""11.1.1 V-Tail Controls""; ""11.1.2 Aircraft Flight Controls""; ""11.1.3 The Airfield""; ""11.2 Ground Effect""; ""11.3 Flight Data Analysis""; ""11.3.1 Anaconda with NACA 0015 Conventional Wing Flight Data""; ""11.3.2 UC2AV Flight Data""; ""11.3.3 Flight Controls""; ""11.3.4 Preflight Data Analysis""; ""11.3.5 Flow Uniformity""; ""11.3.6 Momentum Coefficient of Blowing""; ""11.3.7 Flight Data Analysis""; ""11.4 Remarks""
Control code
on1011253460
Dimensions
unknown
Extent
1 online resource (147 p.)
File format
one file format
Form of item
online
Isbn
9783319678528
Level of compression
unknown
Quality assurance targets
unknown
Reformatting quality
unknown
Specific material designation
remote
System control number
(OCoLC)1011253460
Label
Foundations of circulation control based small-scale unmanned aircraft : a comprehensive methodology from concept to design and experimental testing, Konstantinos Kanistras, Kimon P. Valavanis, Matthew J. Rutherford, (electronic resource)
Publication
Note
  • Description based upon print version of record
  • ""12 Epilogue""
Antecedent source
file reproduced from an electronic resource
Contents
  • ""Preface""; ""Acknowledgements""; ""Contents""; ""Acronyms""; ""1 Introduction""; ""1.1 Background Information""; ""1.2 Motivation""; ""1.3 Introduction to the Problem""; ""1.4 Method of Approach""; ""1.5 Outline of the Research Monograph""; ""2 Aircraft Performance and Design""; ""2.1 Design Considerations""; ""2.1.1 Wing Design""; ""2.1.2 Aircraft Tail Design""; ""2.2 Remarks""; ""3 Fundamentals of Circulation Control""; ""3.1 Vorticity and Circulation""; ""3.1.1 Kevin's and Helmholtz's Vortex Theorems""; ""3.1.2 Finite Wing Theory""; ""3.2 Coand Effect""; ""3.2.1 2-D Analysis""
  • ""3.2.2 Coand Jet Circulation Control""""3.3 Remarks""; ""4 The History of Circulation Control""; ""4.1 Numerical Analysis""; ""4.2 Experimental Work""; ""4.2.1 CC on Full-Scale Aircraft""; ""4.2.2 Circulation Control on Unmanned Aerial Vehicles""; ""4.3 Remarks""; ""5 Airfoil and Flap Design""; ""5.1 Coand Surfaces""; ""5.1.1 Airfoil Shapes""; ""5.1.2 Dual Radius Flap Geometry""; ""5.1.3 CCW Wind Tunnel Model""; ""5.2 Remarks""; ""6 Plenum Design""; ""6.1 Plenum Geometry""; ""6.1.1 Preliminary Plenum Design""; ""6.1.2 Diffuser-Based Plenum Design""; ""6.2 Remarks""; ""7 Instrumentation""
  • ""7.1 Wind Tunnel""""7.2 Force Balance""; ""7.2.1 The Concept""; ""7.2.2 Setup""; ""7.2.3 Calibration""; ""7.3 Pitot Probe""; ""7.4 Remarks""; ""8 Wind Tunnel Results and Discussion""; ""8.1 No Blowing and Blowing Case Comparison""; ""8.1.1 Effect of Blowing on Lift Coefficient CL""; ""8.1.2 Lift-to-Drag Ratio""; ""8.2 NACA 0015 CCW Configuration""; ""8.2.1 Wind Tunnel Test Conditions""; ""8.2.2 Cruise Flight Performance, 0o Flap Deflection""; ""8.2.3 High-Lift Takeoff Performance, 30o Flap Deflection""; ""8.2.4 High-Lift Takeoff Performance, 60o Flap Deflection""
  • ""8.2.5 Further Data Analysis""""8.3 Remarks""; ""9 UC2AV: Unmanned Circulation Control Aerial Vehicle""; ""9.1 The Aircraft""; ""9.2 Air Supply Unit and Air Delivery System""; ""9.2.1 Air Supply Unit""; ""9.2.2 Air Delivery System""; ""9.3 Circulation Control System""; ""9.4 Circulation Control Wing""; ""9.4.1 CCW Structural Analysis""; ""9.4.2 NACA 0015 Wing Implementation""; ""9.4.3 Circulation Control Wing Implementation""; ""9.5 Remarks""; ""10 Aircraft Takeoff Performance""; ""10.1 Takeoff Performance""; ""10.1.1 Takeoff Distance""; ""10.1.2 Pilot Takeoff Technique and Corrections""
  • ""10.1.3 One-at-a-Time Sensitivity Analysis""""10.2 Instrumentation and Sensors""; ""10.3 Remarks""; ""11 Flight Testing""; ""11.1 Aircraft Controls and Data Collection""; ""11.1.1 V-Tail Controls""; ""11.1.2 Aircraft Flight Controls""; ""11.1.3 The Airfield""; ""11.2 Ground Effect""; ""11.3 Flight Data Analysis""; ""11.3.1 Anaconda with NACA 0015 Conventional Wing Flight Data""; ""11.3.2 UC2AV Flight Data""; ""11.3.3 Flight Controls""; ""11.3.4 Preflight Data Analysis""; ""11.3.5 Flow Uniformity""; ""11.3.6 Momentum Coefficient of Blowing""; ""11.3.7 Flight Data Analysis""; ""11.4 Remarks""
Control code
on1011253460
Dimensions
unknown
Extent
1 online resource (147 p.)
File format
one file format
Form of item
online
Isbn
9783319678528
Level of compression
unknown
Quality assurance targets
unknown
Reformatting quality
unknown
Specific material designation
remote
System control number
(OCoLC)1011253460

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