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Fixed and flapping wing aerodynamics for micro air vehicle applications / edited by Thomas J. Mueller.

LIBRA TL507 .P75 v.195
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Format:
Book
Contributor:
Mueller, T. J.
American Institute of Aeronautics and Astronautics.
Series:
Progress in astronautics and aeronautics ; v. 195.
Progress in astronautics and aeronautics ; v. 195
Language:
English
Subjects (All):
Aerodynamics.
Physical Description:
xix, 586 pages : illustrations ; 24 cm.
Place of Publication:
Reston, Va. : American Institute of Aeronautics and Astronautics, 2001.
Summary:
Recently, there has been a serious effort to design aircraft that are as small as possible for special, limited-duration missions. These vehicles may carry visual, acoustic, chemical, or biological sensors for such missions as traffic management, hostage situation surveillance, rescue operations, etc. The goal is to develop aircraft systems that weigh less than 90 grams, with a 15-centimeter wingspan. Since it is not possible to meet all of the design requirements of a micro air vehicle with current technology, research is proceeding. This new book reports on the latest research in the area of aerodynamic efficiency of various fixed wing, flapping wing, and rotary wing concepts. It presents the progress made by over 50 active researchers in the field from Canada, Europe, Japan, and the United States. It is the only book of its kind.
Contents:
Chapter 1 An Overview of Micro Air Vehicle Aerodynamics / Thomas J. Mueller, James D. DeLaurier 1
II. Fixed Wing Vehicles 4
III. Flapping Wing Vehicles 6
Part I. Fixed Wing Aerodynamics
Chapter 2 Higher-Order Boundary Layer Formulation and Application to Low Reynolds Number Flows / Mark Drela 13
II. Curvilinear Coordinates and Equations 15
III. Equivalent Inviscid Flow 16
IV. Entrainment Equation and Viscous/Inviscid Coupling 17
V. Integral Momentum and Kinetic Energy Equations 17
VI. Turbulent Transport Equation 18
VII. Real Viscous Flow Profiles 19
VIII. Profile Families 21
IX. Higher-Order Corrections 22
X. High-Order Panel Method 24
XI. Viscous/Inviscid System Formulation 29
XII. Results 30
Chapter 3 Analysis and Design of Airfoils for Use at Ultra-Low Reynolds Numbers / Peter J. Kunz, Ilan Kroo 35
II. Computational Analysis Methods 36
III. Flowfield Assumptions 38
IV. Grid Topology 39
V. Comparison with Experiment 40
VI. Effects of Reynolds Number and Geometry Variations on Airfoil Performance 41
VII. Airfoil Optimization 56
Chapter 4 Adaptive, Unstructured Meshes for Solving the Navier-Stokes Equations for Low-Chord-Reynolds-Number Flows / J. T. Monttinen, R. R. Shortridge, B. S. Latek, H. L. Reed, W. S. Saric 61
II. Approach 63
III. The Finite Element Approximation 66
IV. Fluid Solver 67
V. Grid Generation and Adaptive Refinement 70
VI. Results 73
VII. Database Validation 76
VIII. Ongoing Work 76
Chapter 5 Wind Tunnel Tests of Wings and Rings at Low Reynolds Numbers / E. V. Laitone 83
II. Effect of Aspect Ratio and Planform on the Aerodynamic Lift and Drag 84
III. Effect of Low Reynolds Numbers on the Lift and Drag of Ring Airfoils 86
Chapter 6 Effects of Acoustic Disturbances on Low Re Aerofoil Flows / T. M. Grundy, G. P. Keefe, M. V. Lowson 91
II. Experimental Arrangements 94
III. Results 98
V. Potential Use of Sound to Improve Performance 110
Chapter 7 Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers / Gabriel E. Torres, Thomas J. Mueller 115
II. Apparatus 117
III. Procedures 119
IV. Uncertainty 120
V. Flow Visualization 120
VI. Discussion of Results 121
VII. Vortex-Lattice Method 137
Chapter 8 Systematic Airfoil Design Studies at Low Reynolds Numbers / Michael S. Selig, Ashok Gopalarathnam, Philippe Giguere, Christopher A. Lyon 143
II. Design Process 144
III. Parametric Studies in Airfoil Design 147
Chapter 9 Numerical Optimization and Wind-Tunnel Testing of Low Reynolds Number Airfoils / Th. Lutz, W. Wurz, S. Wagner 169
II. Aerodynamic Model 171
III. Experimental Setup 172
IV. Numerical Optimization of Low Reynolds Number Airfoils 176
V. Experimental Investigations on Very Low Reynolds Number Airfoils 182
VI. Conclusion and Outlook 188
Chapter 10 Unsteady Stalling Characteristics of Thin Airfoils at Low Reynolds Number / Andy P. Broeren, Michael B. Bragg 191
II. Experimental Methods 193
Part II. Flapping and Rotary Wing Aerodynamics
Chapter 11 Thrust and Drag in Flying Birds: Applications to Birdlike Micro Air Vehicles / Jeremy M. V. Rayner 217
II. Avian Flight Performance 219
III. Thrust Generation 222
IV. Drag Reduction 224
V. Wing Shape 226
Chapter 12 Lift and Drag Characteristics of Rotary and Flapping Wings / C. P. Ellington, J. R. Usherwood 231
II. Aerodynamics of Hovering Insect Flight 232
III. Propeller Experiments at High Re 237
Chapter 13 A Rational Engineering Analysis of the Efficiency of Flapping Flight / Kenneth C. Hall, Steven R. Hall 249
II. The Influence of Wake Roll Up on Flapping Flight 253
III. Minimum Loss Flapping Theory 258
IV. Results 264
Chapter 14 Leading-Edge Vortices of Flapping and Rotary Wings at Low Reynolds Number / Hao Liu, Keiji Kawachi 275
II. Computational Modeling of a Rotary Wing 277
III. Numerical Accuracy 279
IV. Results 279
Chapter 15 On the Flowfield and Forces Generated by a Flapping Rectangular Wing at Low Reynolds Number / Richard Ames, Oliver Wong, Narayanan Komerath 287
II. Previous Work 288
III. Scope of Present Work 290
IV. Experimental Setup 290
V. Wing Motion 291
VI. Velocity Data Planes 291
VII. Velocity Field Data Analysis 293
VIII. Force Measurements 294
IX. Results and Discussion 295
Chapter 16 Experimental and Computational Investigation of Flapping Wing Propulsion for Micro Air Vehicles / K. D. Jones, T. C. Lund, M. F. Platzer 307
II. General Kinematics 308
III. Plunging Airfoils 311
IV. Pitching Airfoils 318
V. Pitching and Plunging Airfoils 320
VI. Airfoil Combinations 324
Chapter 17 Aerodynamic Characteristics of Wings at Low Reynolds Number / Akira Azuma, Masato Okamoto, Kunio Yasuda 341
II. Unsteady Wing Theory 343
III. Experimental Aerodynamics 354
IV. Geometrical Consideration of Blade Element Theory 363
V. Forces and Moments Acting on Beating Wings 374
Chapter 18 A Nonlinear Aeroelastic Model for the Study of Flapping Wing Flight / Rambod F. Larijani, James D. DeLaurier 399
II. Structural Analysis 405
III. Aerodynamic and Inertial Forces and Moments 407
IV. Damping 415
V. Results and Discussion 419
Chapter 19 Euler Solutions for a Finite-Span Flapping Wing / M. F. Neef, D. Hummel 429
II. Numerical Method 432
III. Investigations for Two-Dimensional Flow 433
IV. Investigations for Three-Dimensional Flow 441
Chapter 20 From Soaring and Flapping Bird Flight to Innovative Wing and Propeller Constructions / Rudolf Bannasch 453
II. Bionic Airfoil Construction 454
III. Bionic Propeller 465
Chapter 21 Passive Aeroelastic Tailoring for Optimal Flapping Wings / Kenneth D. Frampton, Michael Goldfarb, Dan Monopoli, Dragan Cveticanin 473
II. Experimental Setup 475
III. Results 477
Chapter 22 Shape Memory Alloy Actuators as Locomotor Muscles / Othon K. Rediniotis, Dimitris C. Lagoudas 483
II. Brief Overview of SMA Actuators 486
III. Thermomechanical Transformation Fatigue of SMA Actuators 488
IV. Adaptive Control of SMA Actuator Wires 491
V. Energy Considerations for SMA Actuators 494
VI. SMA Actuators as Locomotor Muscles for a Biomimetic Hydrofoil 496
Part III. Micro Air Vehicle Applications
Chapter 23 Mesoscale Flight and Miniature Rotorcraft Development / Ilan Kroo, Peter Kunz 503
II. Approach 508
III. Testing 515
Chapter 24 Development of the Black Widow Micro Air Vehicle / Joel M. Grasmeyer, Matthew T. Keennon 519
II. Early Prototypes 519
III. Multidisciplinary Design Optimization 520
IV. Energy Storage 524
V. Motors 525
VI. Micropropeller Design 526
VII. Airframe Structural Design 528
VIII. Avionics 530
IX. Video Camera Payload 531
X. Stability and Control 532
XI. Performance 532
XII. Ground Control Unit 533
Chapter 25 Computation of Aerodynamic Characteristics of a Micro Air Vehicle / Ravi Ramamurti, William Sandberg 537
II. The Incompressible Flow Solver 538
III. Description of the Micro Air Vehicle Model 539
IV. Discussion of Results 540
Chapter 26 Optic Flow Sensors for MAV Navigation / Geoffrey L. Barrows, Craig Neely, Kurt T. Miller 557
II. Optic Flow 557
III. Description of the Optic Flow Sensor 560
IV. Use of Optic Flow for Navigation 566
V. Initial In-Flight Experiments 567
VI. Next-Generation Sensors 571.
Notes:
Includes bibliographical references.
ISBN:
1563475170
OCLC:
48628459

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