航空文献目录速报

20005

中国航空工业发展研究中心

2000年10月

《航空文献目录速报》以不定期方式报导我所最新获得的有关文献，从而实现航空文献资源共享，提高航空文献的利用率，更好地为航空工业服务，促进航空工业的腾飞。

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“速报”上所报导的各类文献我们可随时提供复印件，如读者需要可直接与信息资源部搜集组联系，来函请写索取号、期号和顺序号，以便查找。

中国航空工业发展研究中心信息资源部

2000年10月

附文献著录格式：

期号－－－－9901－001－－－－－－－－－－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－－－－－－

20005-001

ADA 252777

Integration of tools for the design and assessment of high-performance, highly reliable computing

Systems (DAHPHRS) Dec 1991. 236P

20005-002

ADA 358451

Strength and inelastic deformation in shocked polycrystalline silicon carbide

July 10. 1998. 8P

20005-003

ADA 367319

An experimental investigation of tangential blowing to reduce buffet response of the vertical tails

Of anF-15wing tunnel model Volume 1-test results, discussion and correlation Jan 1999. 241P

20005-004

ADA 367849

Future aircraft technology enhancements-block 1. Nov 1997. 125P

20005-005

ADA 368300

Bird strike committee Europe (BSCE). 19th meeting. Madrid, Spain May 1988. 669P

20005-006

ADA 368446

Structural reliability assessment methodology-Why now ? August 1999. 12P

20005-007

ADA 368599

Risk management of an aging KC-130 fleet. August 1999. 22P

20005-008

ADA 368601

The effect of helmet mounted display field-of-view configuration on target acquisition

Sep 1999. 34P

20005-009

ADA 368608

Feb 1998. 10P.

20005-010

ADA 368657

Experimental investigation of vortex-tail interaction on a76/40 degree double-delta wing

April 1999. 19P.

20005-011

ADA 368768

A comparison of intelligent, adaptive, and nonlinear flight control laws. June 1999.12P.

20005-012

ADA 369176

Sensory adaptation effects following exposure to a virtual environment. Sep 1999. 62P.

20005-13

ADA 369156

Comparisons of flight to ground-based pilot-induced oscillation evaluation methods.

May 1999. 203P.

20005-014

ADA 369203

Low cost parachute guidance, navigation, and control. Sep 1999. 137P.

20005-015

ADA 369204

Integration of common module signature code features. July 1997. 24P.

20005-016

ADA 369418

F-111 Bonded panel repair status. April 1999. 37P

20005-017

ADA 369433

The tactical versus strategic role of the C-17: an analysis of operation joint endeavor.

1999. 5P.

20005-018

ADA 369510

Lessons learned on the B-2 training system. March 1997. 24p

20005-019

ADA 369959

u.s. marine corps aircraft corrosion prevention and control program. Oct 1996. 34P

20005-020

ADA 370020

Progress report on methods of analysis applicable to monocoque aircraft structures.

Air service information circular, volume v3 N0.713 May 1939. 50P

20005-021

ADA 370089

An empirical-theoretical method of comparative prediction of airplane performance.

Air service information circular, volume I.No.68 April 1920. 13p.

20005-022

ADA 370377

FAA debris mitigation impact test report . August 1999. 162P.

20005-023

ADA 370418

UAV aeroservoelastic control using redundant microactuators . Aug 1998.7P

20005-024

ADA 370438

Development experimental investigation of technique for pressure field measurements

on helicopter blade. Aug 1999. 21P

20005-025

ADA 370450

Corrosion and widespread fatigue damage of critical aircraft structure . Sep 1997.

253P.

20005-026

ADA 370463

Stealth, the end of dedicated electronic attack aircraft. May 1999. 62p

20005-027

ADA 370491

Fuselage burnthrough protection for increased postcrash occupant survivability: safety

benefit analysis based on past accidents. Sep 1999.170P

20005-028

ADA 370500

Sep 1999. 30P

20005-029

ADA 370533

Structure and modeling of free-surface turbulence . May 1999. 4P

20005-030

ADA 370552

Studies of time-phased vertical and lateral gusts: development of multiaxis one-minus-cosine gust model . Oct 1999. 61P

20005-031

ADA370584

JSASS 13th international sessions in 37th aircraft symposium. Oct 13-15 1999. 180P

20005-032

ADA 370590

Heat damage assessment for naval aircraft composites. Sep. 1999. 190P

20005-033

ADA 370781

Simulation of thrust-vectored aircraft maneuvers in a human centrifuge: model validation and design

For the dynamic environment simulator . Sep 1999. 135P.

20005-034

ADA 371003

AIAA98-2878 Reynold number scaling at transonic speeds. June 1998. 19P

20005-035

ADA 371212

Flight evaluation of communications earplug in the OH-58D helicopter . Part1. Oct 1999. 46P.

20005-036

ADA 371306

Air force aircraft painting and corrosion control .Jan 1996. 35P

20005-037

ADA 371350

Progress in meeting F-22 cost and schedule goals . December 1999. 9P.

20005-038

ADA 371388

Air force research in aero propulsion technology . Dec 1999.6P.

20005-039

ADA 371451

Optimization with variable-fidelity models applied to wing design.(NASA/CR-1999-209826)Dec

1999. 19P.

20005-040

ADA 371500

C-2a flight simulator training device . Feb 1997. 24P

20005-041

ADA 371780

Department of aeronautics and astronautics . Aug 1999. 68P

20005-042

ADA 371942

General flight test theory applied to aircraft modifications. Spring 1999.11p

20005-043

ADA 371994

F-111 stiffener run out #2 parametric study . Oct 1999.52P.

20005-044

ADA 372187

Improving aviation safety performance. Dec. 1999. 12P

20005-045

ADA 372234

Active control of aeroelasticty and internal flows in turbomachinery . Sec.1999.108P

20005-046

ADA 372327

Reducing aircraft quick-turn ground times the European environment.1999. 47P.

20005-047

PB2000-100005

Simulator evaluation on control and display issues for a future regional aircraft

July 1996. 20P

20005-048

PB2000-100019

A symmetrical boundary element formulation for sound transmission through fuselage walls .

-application- Sep 1996. 28P

20005-049

PB2000-100021

A symmetrical boundary element formulation for sound transmission through fuselage walls.

-theory, implementation and test cases- Sep 1996. 21P.

20005-050

PB2000-100028

Gust load condition fatigue tests based on a continuous gust concept . Apr 1997.16P

20005-051

PB2000-100034

Derivation of lateral and vertical gust statistics from in-flight measurements .

Apr 1997. 16P

20005-052

PB2000-100040

Airfoil design and optimization methods: recent progress at NLR . Sep 1996. 23P.

20005-053

PB2000-100042

Determination of transonic unsteady aerodynamic loads to predict the aeroelastic stability

of flight aircraft. June 1997. 16P

20005-054

PB2000-100043

Analysis of computational aeroelastic simulations by fitting time signals . June 1997.17P

20005-055

PB2000-100045

Computation of flow around fighter aircraft . Oct. 1996. 17P

20005-056

PB2000-100059

Design, fabrication and testing of a composite bracket for aerospace applications . Sep 1997

14P

20005-057

PB2000-100061

Fatigue and fracture in an aircraft engine pylon. March 1997. 13P.

20005-058

PB2000-100062

Application of genetic algorithms in the aerospace domain . Sep. 1966. 12P

20005-059

PB2000-100066

A data acquisition system for the RNLAF MLU F-16 requirements and proposal . Sep 1996. 15P

20005-060

PB2000-100068

20005-061

PB2000-100069

Sep.1995 25P

20005-062

PB2000-100076

Aircraft structural health monitoring, prospects for smart solutions from European viewpoint.

Sep. 1997 15P

20005-063

PB2000-100077

Review of aeronautical fatigue investigations in the Netherlands during the period March 1995-

March 1997. June 1997.39P

20005-064

PB2000-100083

Propeller-Wing Interference Effects at Low speed Conditions. March 1996. 22p

20005-065

PB2000-100092

A symmetrical boundary element formation for sound transmission through cabin walls.Jan.1996

23p

20005-066

PB2000-100442

Full Scale glar4e fuselage panel tests.Aug.1996.16p

20005-067

PB2000-100443

Analysis of measured in-flight tail loads. Sep 1996. 17P

20005-068

PB2000-100903

High-intensity radiated fields (HIDF) risk analysis. July 1999. 25P.

20005-069

PB2000-101057

Wind effects on the lateral motion of wake vortices. Nov 1999. 70P.

20005-070

PB2000-101371

The Interfaces between flightcrews and modern flight deck systems . June 1996. 198P

20005-071

PB2000-102379

Full-scale tests of lightweight fragment barriers commercial aircraft. Nov 1999. 15P

20005-072

PB2000-102393

In-Flight Advisor, Phase 1. Dec 1999. 82P

20005-073

AIAA2000-0418

Multidisciplinary High-Fidelity Analysis and Optimization of Aerospace Vehicles, Part 1: Formulation January 2000. 18P

20005-074

NASA CR-195382

Low Noise Research Fan Stage Design March 1995. 58P

20005-075

NASA CR-1998-208952

The Aviation System Analysis Capability Noise Impact Model November 1998. 76P

20005-076

NASA CR-1999-206583

Unsteady Aerodynamics-Subsonic Compressible Inviscid Case August 1999. 80P

20005-077

NASA CR-1999-209338

Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft

June 1999. 64P

20005-078

NASA CR-1999-209406

Advanced Subsonic Technology (AST) Area of Interest (AOI) 6: Develop and Validate Aeroleastic Codes for Turbomachinery September 1999. 60P

20005-078

NASA CR-1999-209547

Modeling of longitudinal unsteady aerodynamics of a wing-tail combination. Sep 1999. 29P.

20005-079

NASA TM-1999-206584

Design and calibration of an airborne multichannel swept-tuned spectrum analyzer .

Oct 1999.18P.

20005-080

NASA TM-1999-206587

Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane .Oct 1999 .224P

20005-081

NASA TM-1999-206586

Estimated benefits of variable-geometry wing camber control for transport aircraft .

Oct 1999 48P .

20005-082

NASA TM-1999-209013

Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

Dec 1999 . 54P

20005-083

NASA TP-1999-209540

Turbulence model comparisons for a high-speed aircraft . Dec 1999. 58P.

20005-084

NASA TP-1999-209541

Navier-stokes simulation of several high-lift reference H configurations . Dec 1999 94P

20005-085

NASA TP-1999-209683

F-16XL-2 supersonic laminar flow control flight test experiment . Dec 1999. 262P

20005-086

NASA TP-1999-209718

Unstructured grid viscous flow simulation over high research technology concept airplane at

High-lift conditions .Nov 1999 32P.