NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
6th AIAA Biennial Flight Test Conference, Hilton Head Island, SC, Aug. 24-26, 1992, Selected PapersTopics presented include training for avionics evaluation, flight testing in the '90s, methodology for the critical evaluation of flight test data, flight testing of an electric powered vehicle, and the flying qualities of a remotely piloted vehicle. Also presented are airspeed calibration using GPS, the design and conduct of a windshear detection flight experiment, the 757 fly-by-wire demonstrator flight test, and an update of the B-52 flight test program.
Document ID
19930027254
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
American Institute of Aeronautics and Astronautics
Date Acquired
August 15, 2013
Publication Date
August 24, 1992
Publication Information
Publication: 6th AIAA Biennial Flight Test Conference
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/MBFT92
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 6th AIAA Biennial Flight Test Conference
Location: Hilton Head, SC
Country: US
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
93A11251
Funding Number(s)
PROJECT: RTOP 505-68-50
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19930027284WorkThe Development of an Airborne Information Management System for Flight Test19930027271WorkDesign and Conduct of a Windshear Detection Flight Experiment19930027272WorkFlight Testing of the Forward Looking Infra-Red (FLIR) Sensor on the Electronic Combat and Reconnaissance (ECR) Tornado19930027273WorkA Regression Method for Comparing Launch Zone Ranges Derived From Different Sources19930027274Work757 Fly-By-Wire Demonstrator Flight Test19930027275WorkIn-Flight Flow Visualization Results From the X-29A Aircraft at High Angles of Attack19930027282WorkIntegrating Test Results With Analysis to Improve Safe Separation Flight Tests19930027283WorkFlight Experience With Lightweight, Low-Power Miniaturized Instrumentation Systems19930027285WorkThe Effects of Use of Civil Airworthiness Criteria on U.S. Air Force Acquisition, Test and Evaluation Practices19930027286WorkThe Enhanced Flight Screener Operational Demonstration Flight Test Program19930027287WorkResearch on the Stability and Control of Soaring Birds19930027281WorkFlight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control19930027288WorkMeasurement of Attachment-Line Location in a Wind-Tunnel and in Supersonic Flight19930027276WorkCorrelation of Forebody Pressures and Aircraft Yawing Moments on the X-29A Aircraft at High Angles of Attack19930027277WorkFlight Test Results From a Supercritical Mission Adaptive Wing With Smooth Variable Camber19930027278WorkSubsonic High-Lift Flight Research on the NASA Transport System Research Vehicle (TSRV)19930027279WorkIntegrated Flight Propulsion Control Research Results Using the NASA F-15 HIDEC Flight Research Facility19930027280WorkPitch Control Margin at High Angle of Attack - Quantitative Requirements (Flight Test Correlation With Simulation Predictions)
No Preview Available