Evaluation of various thrust calculation techniques on an F404 engine
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Evaluation of various thrust calculation techniques on an F404 engine

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Published by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va .
Written in English

Subjects:

  • Airplanes -- Motors -- Thrust.

Book details:

Edition Notes

StatementRonald J. Ray.
SeriesNASA technical paper -- 3001.
ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17677285M

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Get this from a library! Evaluation of various thrust calculation techniques on an F engine. [Ronald J Ray; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.]. In support of performance testing of the XA aircraft at the NASA-Ames, various thrust calculation techniques were developed and evaluated for use on the FGE engine. The engine was thrust calibrated at NASA-Lewis. Results from these tests were used to correct the manufacturer's in-flight thrust program to more accurately calculate thrust for the specific test engine. Data from these . In support of performance testing of the XA aircraft at the NASA-Ames, various thrust calculation techniques were developed and evaluated for use on the FGE engine. The engine was thrust calibrated at NASA-Lewis. Results from these tests were used to correct the manufacturer's in-flight thrust program to more accurately calculate thrust for the specific test engine. Data from these Author: Ronald J. Ray. Evaluation of various thrust calibration [i.e. calculation] techniques on an F engine / By Ronald J. Ray and Dryden Flight Research Facility. Abstract. Title corrected from errata title page issued in May, "April "Prepared at Dryden Flight Research graphy: p. Mode of .

A PRELIMINARY EVALUATION OF AN F ENGINE PARAMETER ESTIMATION PROCESS USING FLIGHT DATA Authors: Trindel A. Maine, Glenn B. Gilyard and Heather H. Lambert Report Number: NASA-TM Performing Organization: NASA Dryden Flight Research Center, Edwards, CA Availability: Format(s) on-line: PDF (1, KBytes) Report Date: August RONALD J RAY, "Evaluation of Various Thrust Calibration Techniques on an F Engine" NASA TP , April Uncertainty in in-flight Thrust Determination, AIR Aug FIN The highest thrust variant of the F family, the -IN20, deploys the latest hot section materials and technologies to power India's Light Combat Aircraft. Download Data Sheet. bleed air extraction effects on engine performance and operability. This paper addresses the measurement of thrust loss during increases in bleed air extraction for an FGE engine installed on the F/A HARV. A compar-ison of the predicted thrust loss provided by an engine computer simulation and the measured values will be Size: 1MB.

In may the United States Navy selected the McDonnell Douglas / Northrop corporation to develop its F/A Hornet fighter aircraft, which was powered by two FGE engines. The first F engine test took place merely 1,5 years later in December Preliminary flight rating tests took place in May and the first flight of a F/A powered by the F commenced in November Turbofan and turbojet engines: database handbook Foreword This book shows the engine data which I have collected in rece nt years, from reference books or web sites (cf. the bibliography on page 59 6). I have tried to compare the sources in order to make these data as reliable as possible, but please feel free to inform me of any Size: 78KB. The F, an engine in the kN thrust category, is an uprated version of GE’s F It powers Boeing’s twin-jet combat aircraft F/A Super Hornet and the electronic warfare version EAG Growler. MTU produces the high-pressure compressor spool and various parts for the F Engine statistics; Specification-GE /RMGED; Application: FC/D: JAS 39 Gripen: A-4S (no afterburner) Max Thrust: 17, lb: 18, lb: 11, Max SFC.