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 IBR’s Using Force Modeling and Control
.-May 9-11,2000 .-7P.
2001-1-020
SAE 2000-01-1696
Head–Up 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
World’s 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: CAA’s 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 Electric’s 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.