Nas111_Section_0...

2.0
Aerodynamic Theories
Aerodynamic Theories In MSC.Nastran
Aerody百度文库amic Matrix Generation
Aerodynamic Model Generation
Aerodynamic Elements
Aerodynamic Grid Points
4.0
Static Aeroelasticity
Static Aeroelasticity Static Aeroelasticity - Theory
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2-84 2-85 2-88 2-89 2-90 2-92 2-98
3-3 3-4 3-6 3-7 3-9 3-11 3-12 3-14 3-15 3-16 3-17 3-18 3-21
Section
2.0
Aerodynamic Theories (Cont.)
Doublet-lattice Method - Theory The N5KQ Option For Doublet Lattice Doublet-lattice Lifting Surface Entry Associated Bodies For The Doublet-lattice Method Input Of Real Numbers For Aerodynamic Analysis Doublet-lattice Method Modeling Guidelines Doublet-lattice Paneling Example ZONA51 ZONA51 - Theory ZONA51 Modeling Guidelines Subsonic Wing-body Interference Theory Subsonic Body Geometry Entry Subsonic Body Properties Wing-body Modeling Guidelines Example Of Lifting Surface/body With Slender Body Elements Special Consideration For Wing/body Interference Alternatives For Bodies Mach Box Method Mach Box Aerodynamic Panel Entry Mach Box Panel Properties Mach Box - Modeling Guidelines Mach Box Example - Mach = 1.3 Strip Theory Strip Theory Aerodynamic Panel Geometry Strip Theory Panel Properties Strip Theory - Modeling Guidelines
3.0
Splines
Interpolation Using Surface Splines Structural/aerodynamic Model Interconnection Surface Splines Surface Spline Options Linear Spline The Surface Spline Data Entry Surface Spline Data Entry & Modeling Guidelines The Linear Spline Data Entry The Spline3 Bulk Data Entry Set1 Bulk Data Entry Set2 Bulk Data Entry Spline Modeling Guidelines Special Cases For The Spline
Section
2.0
Aerodynamic Theories (Cont.)
Strip Theory Example Piston Theory Piston Theory Aerodynamic Panel Entry Piston Theory Panel Properties Piston Theory - Thickness Properties Piston Theory - Modeling Guidelines Aerodynamic Model Generation Summary
NAS111 Course Notes
April 2005
Part Number:NA*V2003*Z*Z*Z*SM-NAS111-NT1
DISCLAIMER
MSC.Software Corporation reserves the right to make changes in specifications and other information contained in this document without prior notice. The concepts, methods, and examples presented in this text are for illustrative and educational purposes only, and are not intended to be exhaustive or to apply to any particular engineering problem or design. MSC.Software Corporation assumes no liability or responsibility to any person or company for direct or indirect damages resulting from the use of any information contained herein. User Documentation: Copyright© 2003 MSC.Software Corporation. Printed in U.S.A. All Rights Reserved. This notice shall be marked on any reproduction of this documentation, in whole or in part. Any reproduction or distribution of this document, in whole or in part, without the prior written consent of MSC.Software Corporation is prohibited. MSC and MSC. are registered trademarks and service marks of MSC.Software Corporation. NASTRAN is a registered trademark of the National Aeronautics and Space Administration. MSC.Nastran is an enhanced proprietary version developed and maintained by MSC.Software Corporation. MSC.Patran is a trademark of MSC.Software Corporation. All other trademarks are the property of their respective owners.
TABLE OF CONTENTS
Section
1.0
Introduction
Introduction To Aeroelastic Analysis In MSC.Nastran Aeroelasticity The Aeroservoelastic Triangle Aeroelastic Phenomena Bibliography On Aeroelasticity History Of Aeroelastic Capability In MSC.Nastran The Four Aeroelastic Solutions In MSC.Nastran MSC Documentation Useful For Aeroelasticity MSC.Nastran CONCEPTS Solution Sequences Related To Aeroelasticity Matrix And Vector Notation Other Notation Used Hierarchy Of Displacement Sets Relation Of Dynamic Analysis Sets Aerodynamic And Solution Sets Bulk Data Entries And Associated Sets Coordinate Systems Coordinate Systems In Aeroelasticity
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MSC.Nastran Aeroelastic Analysis
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2-27 2-30 2-32 2-33 2-34 2-35 2-39 2-41 2-43 2-46 2-49 2-55 2-57 2-59 2-62 2-63 2-65 2-67 2-70 2-71 2-73 2-75 2-76 2-78 2-79 2-80
TABLE OF CONTENTS
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Tel: (714) 540-8900 Fax: (714) 784-4056 Web: http://www.mscsoftware.com
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4-4 4-5
TABLE OF CONTENTS
Section
4.0
Static Aeroelasticity (Cont.)
Corrections To The MSC.Nastran Aeroelastic Analysis User’s Guide Static Aeroelastic Trim Analysis Divergence Analysis Aeroelastic Stability Derivatives Correction Factors For Static Aeroelasticity Summary Of Input Unique To Static Aeroelastic Response AECONFIG AESYMXZ AESYMXY AEROF APRESSURE TRIM DIVERG Static Aeroelastic Parameters Data Entry Remarks For The AEROS Entry Restrictions On Coordinate Systems Rigid Body Motion Data Entry Remarks For The AESTAT Entry Control Surface Data Entry AELIST Bulk Data Entry Flight Condition Specification Further Remarks For The Trim Entry Linking Of Aerodynamic Extra Points Divergence Condition Specification The PARAM Bulk Data Entry User Aerodynamic Input And Correction Examples Output For Static Aeroelasticity
Doublet-lattice Method
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1-4 1-5 1-7 1-8 1-17 1-21 1-24 1-25 1-28 1-29 1-30 1-31 1-32 1-33 1-34 1-35 1-36 1-37
2-5 2-19 2-20 2-21 2-23 2-24
TABLE OF CONTENTS