Single-stage experimental evaluation of boundary layer bleed techniques for high lift stator blades. Compressors design
Design and evaluation of stator blades for use in boundary layer bleed techniques in axial flow compressor
Chapman, D. C.↗
SEARCH · Search NASA
Results for “Compressor”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Friction and wear under fretting conditions of materials for use as wire friction dampers of compressor blade vibration
Friction and fretting wear tests on materials used as friction dampers to reduce vibrational stresses in compressor blades for turbine engines
Johnson, R. L.↗
Development of compressor end seals, stator interstage seals, and stator pivot seals in advanced air-breathing propulsion systems Semiannual report, 1 Jul. - 31 Dec. 1967
Development of compressor, stator, and vane pivot seals for use in advanced air breathing engines
Hawkins, R. M.↗
Noise reduction by means of inlet-guide-vane choking in an axial-flow compressor
Inlet guide vane choking noise reduction in axial flow compressors
Chestnutt, D.↗
Overall performance in argon of a 6-inch radial-bladed centrifugal compressor
Overall performance tests in argon of six inch radial bladed centrifugal compressor
Ball, C. L.↗
Saturn telemetry data compressor test program Final report
Saturn pulse frequency modulation telemetry data processed through predictor data compressor
Labmeier, C. D.↗
Axial flow compressor design computer programs incorporating full radial equilibrium. Part 2 - Radial distribution of total pressure and flow path or axial velocity ratio specified /program 3/
Axial flow compressor design computer programs incorporating radial distribution of total pressure and flow path or axial velocity ratio
Carmody, R. H.↗
Design of floated shoe close clearance seals for supersonic jet engine compressors.
Floated shoe close running air seals for supersonic jet engine compressors, discussing axial and radial seals design
Cheng, H.↗
The prevention of transmission buffer overflow in telemetry data compressors.
Transmission buffer overflow prevention in telemetry data compressors using adaptive queueing control system
Medlin, J. E.↗
Design of one-piece jet-engine compressor end seals.
One piece face type flexible and rigid seals designed for compressor end area of air breathing propulsion systems, based on gas bearing
Thorkildsen, R. L.↗
Configurations for gas turbine compressor end seals.
Gas turbine compressor end seals, discussing air leakage paths, primary and secondary seals, design and efficiency
Bjerklie, J. W.↗
Computer programs for axial flow compressor design
Four computer programs examine effects of design parameters and indicate areas for research of multistage axial flow compressors. The programs provide information on velocity diagrams and stage-by-stage performance calculation, radial equilibrium of flow, radial distribution of total pressure, and off-design performance calculation.
Carmody, R. H.↗
Axial flow compressor computer program for calculating off design performance /Program 4/
Computer program for calculating off-design aerodynamic performance of axial flow compressor
Carmody, R. H.↗
Compressor noise analysis
Prediction method for noise radiation from turbojet compressor fan
Lowson, M. V.↗
Performance comparisons of high Mach number compressor rotor blading
Performance comparisons of supersonic compressor rotor blades
Gostelow, J. P.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 3 - Performance of blowing insert configuration no. 1
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and performance tests using distorted or undistorted inlet flow
Koch, C. C.↗
A survey of salt deposits in compressors of flight gas turbine engines
Analysis of sodium chloride deposits on compressor blades of flight gas turbine engines
Ashbrook, R. L.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 4 - Performance of bleed insert configuration no. 3
Evaluation of bleed insert configuration of single stage axial flow compressor
Koch, C. C.↗