Nasa Technical Note

Author:
Editor:
ISBN:
File Size: 12,64 MB
Format: PDF, Mobi
Read: 8505
Download


Effects Of Diffusion Factor Aspect Ratio And Solidity On Overall Performance Of 14 Compressor Middle Stages

Author: Werner R. Britsch
Editor:
ISBN:
File Size: 55,15 MB
Format: PDF, ePub, Docs
Read: 9599
Download


Nasa Technical Note

Author: United States. National Aeronautics and Space Administration
Editor:
ISBN:
File Size: 10,90 MB
Format: PDF, ePub, Mobi
Read: 1903
Download


Mission Oriented R D And The Advancement Of Technology

Author: Martin D. Robbins
Editor:
ISBN:
File Size: 20,47 MB
Format: PDF, Kindle
Read: 1529
Download


Overall And Blade Element Performance Of A 1 20 Pressure Ratio Fan Stage At Design Blade Setting Angle

Author: George W. Lewis (Jr.)
Editor:
ISBN:
File Size: 43,95 MB
Format: PDF, ePub
Read: 2420
Download


Overall And Blade Element Performance Of A 1 20 Pressure Ratio Fan Stage With Rotor Blades Reset 5

Author: George W. Lewis (Jr.)
Editor:
ISBN:
File Size: 27,26 MB
Format: PDF, Docs
Read: 8985
Download

A 51-cm-diam model of a fan stage for a short haul aircraft was tested in a single stage-compressor research facility. The rotor blades were set 5 deg toward the axial direction (opened) from design setting angle. Surveys of the air flow conditions ahead of the rotor, between the rotor and stator, and behind the stator were made over the stable operating range of the stage. At the design speed of 213.3 m/sec and a weight flow of 31.5 kg/sec, the stage pressure ratio and efficiency were 1.195 and 0.88, respectively. The design speed rotor peak efficiency of 0.91 occurred at the same flow rate.

A Collection Of Technical Papers

Author:
Editor:
ISBN:
File Size: 56,34 MB
Format: PDF, Kindle
Read: 9210
Download


Performance Of Low Pressure Ratio Low Tip Speed Fan Stage With Blade Tip Solidity Of 0 65

Author: George Kovich
Editor:
ISBN:
File Size: 48,99 MB
Format: PDF, Docs
Read: 5942
Download

The overall and blade-element performance of a low pressure ratio, low tip speed fan stage is presented over the stable operating range at rotative speeds from 90 to 120 percent of design speed. Stage peak efficiency of 0.927 was obtained at a weight flow of 32.4 kg sec (190.31 kg sec sq m of annulus area) and a pressure ratio of 1.134. The stall margin at design speed and peak efficiency was 15.3 percent.

Performance Of A 1 15 Pressure Ratio Axial Flow Fan Stage With A Blade Tip Solidity Of 0 5

Author: Walter Martin Osborn
Editor:
ISBN:
File Size: 50,40 MB
Format: PDF, Mobi
Read: 4706
Download


Sae Quarterly Transactions

Author: Society of Automotive Engineers
Editor:
ISBN:
File Size: 60,31 MB
Format: PDF, ePub
Read: 6804
Download


Centrifugal Compressors

Author: SAE Powerplant Activity Committee
Editor:
ISBN:
File Size: 53,32 MB
Format: PDF, Docs
Read: 5736
Download


Performance Prediction And Preliminary Design Of Wave Rotors Enhancing Gas Turbine Cycles

Author: Pezhman Akbari
Editor:
ISBN:
File Size: 59,54 MB
Format: PDF, Mobi
Read: 1084
Download


Paper

Author:
Editor:
ISBN:
File Size: 63,99 MB
Format: PDF, ePub, Docs
Read: 820
Download


Two Stage Fan 2 Data And Performance With Redesigned Second Stage Rotor Uniform And Distorted Inlet Flows

Author:
Editor:
ISBN:
File Size: 29,78 MB
Format: PDF, Kindle
Read: 8611
Download


Design And Performance Of A High Pressure Ratio Highly Loaded Axial Flow Transonic Compressor Space

Author: George W. Lewis (Jr.)
Editor:
ISBN:
File Size: 65,44 MB
Format: PDF, Mobi
Read: 8933
Download


Rotor Tip Clearance Effects On Overall And Blade Element Performance Of Axial Flow Transonic Fan Stage

Author: Royce D. Moore
Editor:
ISBN:
File Size: 13,63 MB
Format: PDF, Docs
Read: 1141
Download


Sae Technical Paper Series

Author:
Editor:
ISBN:
File Size: 62,39 MB
Format: PDF, ePub
Read: 2359
Download

Online version: Technical papers portion of the SAE Digital Library references thousands of SAE Technical Papers covering the latest advances and research in all areas of mobility engineering including ground vehicle, aerospace, off-highway, and manufacturing technology. Sample coverage includes fuels and lubricants, emissions, electronics, brakes, restraint systems, noise, engines, materials, lighting, and more. Your SAE service includes detailed summaries, complete documents in PDF, plus document storage and maintenance

Analysis Of An Advanced Technology Subsonic Turbofan Incorporating Revolutionary Materials

Author:
Editor:
ISBN:
File Size: 16,20 MB
Format: PDF, Docs
Read: 496
Download


Reports And Memoranda

Author:
Editor:
ISBN:
File Size: 20,96 MB
Format: PDF, ePub
Read: 2855
Download

Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.

Technical Report

Author: Aeronautical Research Council (Great Britain)
Editor:
ISBN:
File Size: 40,34 MB
Format: PDF, ePub
Read: 6965
Download

Includes its Reports, which are also issued separately.