EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book Guidelines for Characterization of Gas Turbine Engine Total Pressure Planar Wave and Total Temperature Inlet Flow Distortion

Download or read book Guidelines for Characterization of Gas Turbine Engine Total Pressure Planar Wave and Total Temperature Inlet Flow Distortion written by S-16 Turbine Engine Inlet Flow Distortion Committee and published by . This book was released on 2021 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The turbine-engine-inlet flow distortion descriptors summarized in this document apply to the effects of inlet total-pressure, planar-wave, and total-temperature distortions. Guidelines on stability margin, destabilizing influences, types and purposes of inlet data, AIP definition, and data acquisition and handling are summarized from AIR5866, AIR5867, ARP1420, and AIR1419. The degree to which these recommendations are applied to a specific program should be consistent with the complexity of the inlet/engine integration. Total-pressure distortion is often the predominant destabilizing element that is encountered and is often the only type of distortion to be considered, i.e, not all types of distortion need to be considered for all vehicles. The SAE S-16 Turbine Engine Inlet Flow Distortion Committee has developed an Aerospace Recommended Practice (ARP) and Aerospace Information Reports (AIR) describing measurement stations and techniques, and descriptors for different types of inlet total-pressure, planar-wave, and total-temperature distortion. There has been broad acceptance of these descriptors by the industry. Although a treatment for swirl distortion has been proposed, no methodology for swirl distortion has gained wide acceptance. When an accepted methodology exists for swirl distortion, this document will be updated to include it. This document provides a single source that contains the recommended measurement stations and techniques, and descriptors for total-pressure, planar-wave, and total-temperature inlet distortion.

Book Inlet Total Pressure Distortion Considerations for Gas Turbine Engines

Download or read book Inlet Total Pressure Distortion Considerations for Gas Turbine Engines written by S-16 Turbine Engine Inlet Flow Distortion Committee and published by . This book was released on 2011 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Gas Turbine Engine Inlet Flow Distortion Guidelines

Download or read book Gas Turbine Engine Inlet Flow Distortion Guidelines written by S-16 Turbine Engine Inlet Flow Distortion Committee and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects continue to develop and, therefore, periodic updates are anticipated. The effects of other forms of distortion on flow stability and performance, and of any distortion on aeroelastic stability are not addressed.The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems. The degree to which guidelines for descriptor use, assessment techniques, and testing outlined in this document are applied to a specific program should be consistent with the expected severity of the compatibility problem. This document provides definitions of stability margin and total-pressure distortion descriptors for gas turbine engines. In addition, guidelines for stability assessments, testing, instrumentation, data acquisition, and data processing are addressed.This document contains information that is fundamental to the discipline of inlet-engine compatibility and is expected to remain stable for the foreseeable future.

Book Analysis of Total pressure Loss and Airflow Distribution for Annular Gas Turbine Combustors

Download or read book Analysis of Total pressure Loss and Airflow Distribution for Annular Gas Turbine Combustors written by Robert R. Tacina and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computer analysis of total pressure loss and air flow distribution in annular flow gas turbine combustion chambers.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1981 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Design Fabrication and Test of a Gas Turbine Engine and Wave Rotor Test Bed

Download or read book Design Fabrication and Test of a Gas Turbine Engine and Wave Rotor Test Bed written by John Charles Quackenbush and published by . This book was released on 2008 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Steady state Pressure Distortion on Inlet Flow to a High bypass ratio Turbofan Engine

Download or read book Effect of Steady state Pressure Distortion on Inlet Flow to a High bypass ratio Turbofan Engine written by Ronald H. Soeder and published by . This book was released on 1982 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experiments were conducted to determine the effects of steady-state circumferential-pressure distortion on inlet flow and internal engine performance of a high-bypass-ratio turbofan engine. To measure these effects, flow-angle, static-pressure, and total-pressure instrumentation was placed between the rotatable distortion-generator assembly and the engine inlet. In addition, both static-pressure and total-pressure were recorded at the fan exit and compressor inlet and exit. Three circumferential screens were separately mounted on the rotatable assembly. For all configurations data were recorded at each of twelve 30 deg increments of assembly rotation. Experiments were conducted with fan speeds (corrected to station 2 temperature) of 80 or 90 percent of rated condition (7005 rpm) and Reynolds number indices of 0.2 or 0.5. Yaw angle increased between the distortion-generating assembly and the engine inlet. A change in Reynolds number index (RNI) has only a slight effect and a change in speed had no effect on yaw angle distribution. The flow angle was largest in the hub region of the engine inlet.

Book Engine Response to Distorted Inflow Conditions

Download or read book Engine Response to Distorted Inflow Conditions written by and published by . This book was released on 1987 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Analysis of a Gas Turbine boot Strap

Download or read book Experimental Analysis of a Gas Turbine boot Strap written by Hideyoshi Nakamura and published by . This book was released on 1948 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effect of Pressure Ratio and Inlet Pressure on Performance of Experimental Gas Turbine at Inlet Temperature of 800 Degrees R

Download or read book Effect of Pressure Ratio and Inlet Pressure on Performance of Experimental Gas Turbine at Inlet Temperature of 800 Degrees R written by Robert C. Kohl and published by . This book was released on 1948 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1987 with total page 1258 pages. Available in PDF, EPUB and Kindle. Book excerpt: