航空文献目录速报

2001-1

中国航空工业发展研究中心

2001年3月

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中国航空工业发展研究中心信息资源部

2000年12月

附文献着录格式:

期号2001-1-001顺序号

索取号SAE 965503

题名Aircraft vacuum waste system

air flow analysis.-1996.10.14P页数

出版时间

 

2001-1-001

SAE 1999-01-5596

System Integration Based on Reverse Engineering Processes and Digital Mockup for Upgrades of Military Aircrafts. - October 19-21, 1999. 12P.

2001-1-002

SAE 2000-01-1662

Estimating the Rate of Technology Adoption for Cockpit Weather Information Systems. - May 9-11,2000 .-14P.

2001-1-003

SAE 2000-01-1666

Validation of a Crack Initiation Life Analysis Procedure.-May 9-11,2000 .-22P.

2001-1-004

SAE 2000-01-1668

GV Heated Cabin Window Design, Testing, and Certification .-May 9-11,2000.-7P.

2001-1-005

SAE 2000-01-1671

Propeller Installation And Certification Considerations for Small Aircraft.-May 9-11,2000 .-12P.

2001-1-006

SAE 2000-01-1673

Design and Test of an Improved Crashworthiness Small Composite Airframe.-May 9-11,2000 .-18P.

2001-1-007

SAE 2000-01-1674

Dynamic Analysis of Crew Seats and Cockpit Interiors.-May 9-11,2000 .-8P.

2001-1-008

SAE 2000-01-1676

Flying Qualities Evaluation of a Commuter Aircraft with an Ice Contaminated Tailplane .-May 9-11,2000 .-12P.

2001-1-009

SAE 2000-01-1677

The Rise and Fall of General Aviation An Economists View with Focus on Single Engine Aircraft and the Impact of Airline Deregulation.-May 9-11,2000 .-21P.

2001-1-010

SAE 2000-01-1678

Aerodynamics of the Bell P-39 Airacobra and P-63 Kingcobra.-May 9-11,2000 .-15P.

2001-1-011

SAE 2000-01-1679

Beech AT-10 Wichita.-May 9-11.2000 .-11P.

2001-1-012

SAE 2000-01-1683

Collection Efficiency and Ice Accretion Characteristics of Two Full Scale and One 1/4 Scale Business Jet Horizontal Tails.-May 9-11,2000 .-29P.

2001-1-013

SAE 2000-01-1685

Evaluation of an Unconventional Diesel Engine as a General Aviation Powerplant.-May 9-11,2000 .-8P.

2001-1-014

SAE 2000-01-1686

A New Approach to the Design of a Diesel Engine for General Aviation Aircraft Propulsion.-May 9-11,2000 .-15P.

2001-1-015

SAE 2000-01-1690

NASA/SATS Life Cycle Cost Model.-May 9-11,2000 .-15P.

 

2001-1-016

SAE 2000-01-1691

Spin Resistance Development for Small Airplanes A Retrospective.-May 9-11,2000

.-29P.

2001-1-017

SAE 2000-01-1692

Method of Determining Propeller Pitch Stops for a FAR 23 Airplane.-May 9-11,2000 .-7P.

2001-1-018

SAE 2000-01-1693

Flap Sizing for Wake Vortex Instability.-May 9-11,2000 .-11P.

2001-1-019

SAE 2000-01-1694

Increasing Productivity in 5-Axis Milling of IBRs Using Force Modeling and Control

.-May 9-11,2000 .-7P.

2001-1-020

SAE 2000-01-1696

HeadUp and Head-Down Display Test and Evaluation.-May 9-11,2000 .-13P.

2001-1-021

SAE 2000-01-1697

A Head-Up Display for General Aviation.-May 9-11,2000 .-12P.

2001-1-022

SAE 2000-01-1698

IAR-46 JAR-VLA International Certification.-May 9-11,2000 .-6P.

2001-1-023

SAE 2000-01-1699

Simulation of Aircraft Landing Gear Dynamics Using CATIA, CATDADS, DADS and NASTRAN at Cessna Aircraft.-May 9-11,2000 .-7P.

2001-1-024

SAE 2000-01-1700

Preliminary Estimation of Airplane Moments of Inertia Using CAD Solid Modeling.-May 9-11,2000 .-8P.

2001-1-025

SAE 2000-01-1704

Strategies for Implementing an Error Management Program into General Aviation Organizations.-May 9-11,2000 .-9P.

2001-1-026

SAE 2000-01-1705

Promoting More Effective Communication of Maintenance Issues Between Pilots and Maintenance Technicians.-May 9-11,2000 .-15P.

2001-1-027

SAE 2000-01-1706

Industry Survey Results: Implications for Communication of Critical Aircraft Information Between Pilots and Maintenance Technicians.-May 9-11,2000 .-9P.

2001-1-028

SAE 2000-01-1707

Optimizing Sensor and Actuator Arrays for ASAC Noise Control.-May 9-11,2000 .-12P.

2001-1-029

SAE 2000-01-1708

Aircraft Engine Attachment and Vibration Control.-May 9-11,2000 .-13P.

2001-1-030

SAE 2000-01-1709

Interior Noise Source/Path Identification Technology.-May 9-11,2000 .-11P.

2001-1-031

SAE 2000-01-1710

The Development of Non-Hydraulic Shimmy Dampers.-May 9-11,2000 .-8P

 

2001-1-032

SAE 2000-01-1712

Design of Ethanol Based Fuels for Aviation.-May 9-11,2000 .-16P.

2001-1-033

SAE 2000-01-1714

The Multi-Fuel General Aviation Piston Engine.-May 9-11,2000 .-28P.

2001-1-034

SAE 2000-01-5500

MICCO Mac-145B Spin Flight Test.-October 10-12,2000 .-9P.

2001-1-035

SAE 2000-01-5501

Certification Flight Test for an Extended Range Modification for the Cessna 337 Aircraft.-October 10-12,2000 .-7P.

2001-1-036

SAE 2000-01-5502

The Bombardier Flight Test Center-Meeting the Challenge.-October 10-12,2000 .-20P.

2001-1-037

SAE 2000-01-5503

Next Generation European Air System.-October 10-12,2000 .-5P.

2001-1-038

SAE 2000-01-5505

Military Pilot Training Concepts.-October 10-12,2000 .-10P.

2001-1-039

SAE 2000-01-5507

The Sunriser-A Design Study in Solar Powered Flight.-October 10-12,2000 .-10P.

2001-1-040

SAE 2000-01-5510

An Experimental and Theoretical Study of Reynolds and Mach Number Effects at Two-Dimensional Wind Tunnel Testing.-October 10-12,2000 .-9P.

2001-1-041

SAE 2000-01-5511

Wake Flow in an Adverse Pressure Gradient.-October 10-12,2000 .-11P.

2001-1-042

SAE 2000-01-5514

Lessons Learned from the British Aircraft Corporation TSR2 Project.-October 10-12,2000 .-15P.

2001-1-043

SAE 2000-01-5515

Worlds First Delta Wing Airplane Convair/Air Force XF-92A.-October 10-12,2000 .-11P.

2001-1-044

SAE 2000-01-5516

Specialized Anti-Armor Aircraft of the Eastern Front: 1941-1945.-October 10-12,2000 .-17P.

2001-1-045

SAE 2000-01-5517

The Clark Y Airfoil: A Historical Retrospective.-October 10-12,2000 .-23P.

2001-1-046

SAE 2000-01-5518

Augmentation for Synthetic Vision Displays � An Energy Based Approach.-October 10-12,2000 .-10P.

2001-1-047

SAE 2000-01-5520

Initial Evaluation of CDTI/ADS-B for Commercial Carriers: CAAs Ohio Valley Operational Evaluation.-October 10-12,2000 .-18P.

2001-1-048

SAE 2000-01-5521

Integration of Cockpit Displays for Surface Operations: The Final Stage of a Human-Centered Design Approach.-October 10-12,2000 .-15P.

2001-1-049

SAE 2000-01-5522

A Glass Cockpit Crew Activity Analysis Tool.-October 10-12,2000 .-8P.

2001-1-050

SAE 2000-01-5523

Propulsion Flight Testing on General Electrics B747 Flying Test Bed.- October 10-12,2000 .-8P.

2001-1-051

SAE 2000-01-5525

Scenario-Based Systems Studies for Military Aircraft.- October 10-12,2000 .-10P.

2001-1-052

SAE 2000-01-5527

An Exergy-Based Methodology for Decision-Based Design of Integrated Aircraft Thermal Systems.- October 10-12,2000 .-12P.

2001-1-053

SAE 2000-01-5534

Modeling and Design of Piezoelectric Actuators for Fluid Flow Control.- October 10-12,2000 .-10P.

2001-1-054

SAE 2000-01-5535

1998/1999 AIAA Foundation Graduate Team Aircraft Design Competition: Super STOL Carrier On-board Delivery Aircraft.-October 10-12,2000 .-18P.

2001-1-055

SAE 2000-01-5536

A Student Developed Sizing Methodology for Electric Powered Aircraft Applied to Small UAVs.-October 10-12,2000 .-5P.

2001-1-056

SAE 2000-01-5538

Design of a High-g Unmanned Aerial Vehicle Structure.-October 10-12,2000 .-9P.

2001-1-057

SAE 2000-01-5542

Costs and Benefits of Head up Displays: An Attention Perspective and a Meta Analysis.-October 10-12 .-8P.

2001-1-058

SAE 2000-01-5543

The Fundamentals of Performance Based Training in Aviation.-October 10-12,2000 .-9P.

2001-1-059

SAE 2000-01-5544

An Applied Program of Aviation Safety Training for the Civil Aviation Flying College of China.-October 10-12,2000 .-5P.

2001-1-060

SAE 2000-01-5545

Intelligent Tutoring Systems for Aviation Automation.-October 10-12,2000 .-13P.

2001-1-061

SAE 2000-01-5546

Aircraft Design Optimizing Operators, Environmental System and Manufacturers Requirements.-October 10-12,2000 .-11P.

2001-1-062

SAE 2000-01-5547

Regional Aircraft Family Design.-October 10-12,2000 .-11P.

2001-1-063

SAE 2000-01-5549

Research Programs for Transport Aircraft in Europe.-October 10-12,2000 .-11P.

2001-1-064

SAE 2000-01-5552

Redesign of the C-17 Globemaster III Auxiliary Power Unit (APU) Exhaust System.-October 10-12,2000 .-8P.

2001-1-065

SAE 2000-01-5559

Formulation, Realization, and Demonstration of a Process to Generate Aerodynamic Metamodels for Hypersonic Cruise Vehicle Design.-October 10-12,2000 .-12P.

2001-1-066

SAE 2000-01-5560

A Method for Concept Exploration of Hypersonic Vehicles in the Presence of Open & Evolving Requirements.-October 10-12,2000 .-15P.

2001-1-067

SAE 2000-01-5561

Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter.-October 10-12,2000 .-10P.

2001-1-068

SAE 2000-01-5562

A Generalized Model for Vehicle Thermodynamic Loss Management and Technology Concept Evaluation.-October 10-12,2000 .-14P.

2001-1-069

SAE 2000-01-5563

A Method for Technology Selection Based on Benefit, Available Schedule and Budget Resources.-October 10-12,2000 .-17P.

2001-1-070

SAE 2000-01-5564

A Parametric Design Environment for Including Signatures Analysis in Conceptual Design.-October 10-12,2000 .-16P.

2001-1-071

SAE 2000-01-5565

An Automated Robust Process for Physics Based Aerodynamic Prediction.-October 10-12,2000 .-14P.

 

2001-1-072

SAE 2000-01-5570

The Low-Altitude Wind Shear and Its Influence Upon Hedgehopping.-October 10-12,2000 .-6P.

2001-1-073

SAE 2000-01-5571

Is PED(Personal Electric Devices) Harmful for the Aircraft?.-October 10-12,2000 .-6P.

2001-1-074

SAE 2000-01-5572

Realization of a Shapevariable Fowler Flap for Transport Aircraft.-October 10-12,2000 .-11P.

2001-1-075

SAE 2000-01-5573

Information Requirements for Traffic Awareness in the Free-flight Environment.-October 10-12,2000 .-14P.

2001-1-076

SAE 2000-01-5574

Enabling Strategic Flight Deck Route Re-Planning Within A Modified ATC Environment: The Display of 4-D Intent Information on a CSD.-October 10-12,2000 .-28P.

2001-1-077

SAE 2000-01-5575

A Computerized Analysis of ATC Tracking Data for an Operational Evaluation of CDTI/ADS-B Technology.-October 10-12,2000 .-11P.

2001-1-078

SAE 2000-01-5576

Pilot-In-The-Loop Evaluation of Cockpit Assistance for Autonomous Operations .-October 10-12,2000 .-13P.

2001-1-079

SAE 2000-01-5577

Benefits of Door-to-Door Travel Time Reduction to US Economy.-October 10-12,2000 .-12P.

2001-1-080

SAE 2000-01-5578

The C-17 Global Air Traffic Management(GATM) Application.-October 10-12,2000 .-7P.

2001-1-081

SAE 2000-01-5579

Solution of an Engine Inlet Compatibility Problem During C-17 Low Cost N/EAT Nacelle Thrust Reverser Development.-October 10-12,2000 .-14P.

2001-1-082

SAE 2000-01-5585

Fasteners Modeling for MSC. Nastran Finite Element Analysis.-October 10-12,2000 .-18P.

2001-1-083

SAE 2000-01-5586

Impact Simulation of Simplified Structural Models of Aircraft Fuselage.-October 10-12,2000 .-8P.

2001-1-084

SAE 2000-01-5589

Methodology for Assessing Survivability Tradeoffs in the Preliminary Design Process.-October 10-12,2000 .-12P.

2001-1-085

SAE 2000-01-5590

Use of Flight Simulation in Early Design: Formulation and Application of the Virtual Testing and Evaluation Methodology.-October 10-12,2000 .-13P.

2001-1-086

SAE 2000-01-5593

Optimal and Near-Optimal Take-off Maneuvers in the Presence of Windshear.-October 10-12,2000 .-13P.

2001-1-087

SAE 2000-01-5594

The Three Facets of Risk.-October 10-12,2000 .-16P.

2001-1-088

SAE 2000-01-5595

Identifying Flight Deck Automation Issues.-October 10-12,2000 .-10P.

2001-1-089

SAE 2000-01-5596

Automation Issues: Perspectives from the Flight Deck.-October 10-12,2000 .-9P.

2001-1-090

SAE 2000-01-5598

Developing a Pilot-Centered Autoflight Interface.-October 10-12,2000 .-6P.

2001-1-091

SAE 2000-01-5599

Reducing Aircraft Brake Squeal with a Damped Brake-Rod.-October 10-12,2000 .-6P.

2001-1-092

SAE 2000-01-5600

Development of the Modeling Environment for the Simulation of an Aircraft Hydraulic System.-October 10-12,2000 .-8P.

2001-1-093

SAE 2000-01-5601

Sizing the Landing Gear in the Conceptual Design Phase.-October 10-12,2000 .-9P.

2001-1-094

SAE 2000-01-5602

An Early TSTO Fully Reusable Vehicle Design Used to "Calibrate" Stage 1 Combined-Cycle Hypersonic Propulsion Systems.-October 10-12,2000 .-22P.

2001-1-095

SAE 2000-01-5605

A Two Stage-to-Orbit High Staging Mach Number Design Concept.-October 10-12,2000 .-16P.

2001-1-096

SAE 2000-01-5609

The Role of Constraints in the MDO of a Cantilever and Strut-Braced Wing Transonic Commercial Transport Aircraft.-October 10-12,2000 .-13P.

2001-1-097

SAE 2000-01-5610

Integration of Configuration Design and Multidisciplinary Analysis of Aircraft.-October 10-12,2000 .-7P.

2001-1-098

SAE 2000-01-5612

Framework for the Assessment of Capacity and Throughput Technologies.-October 10-12,2000 .-14P.

2001-1-099

SAE 2000-01-5614

Staying Ahead of the Automation: A Vertical Situation Display Can Help.-October

10-12,2000 .-11P.

2001-1-100

SAE 2000-01-5615

Displaying the FMS Vertical Profile.-October 10-12,2000 .-7P.

2001-1-101

SAE 2000-01-5616

FMS 3-Dimensional Flight Path Display.-October 10-12,2000 .-8P.