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Cover image for Evaluation of MARC for the analysis of rotating composite blades

Evaluation of MARC for the analysis of rotating composite blades

Location Call # Status
Joyner - Microforms B300 NAS 1.15:4423 ✔ Available
Cover image for Design and integration of a rotor alone nacelle for acoustic fan testing

Design and integration of a rotor alone nacelle for acoustic fan testing

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Cover image for Design and integration of a rotor alone nacelle for acoustic fan testing

Design and integration of a rotor alone nacelle for acoustic fan testing

  • 2001
  • Format: Microform
Location Call # Status
Joyner - Microforms B300 NAS 1.15:210820 ✔ Available
Cover image for Shape Changing Airfoil

Shape Changing Airfoil

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Cover image for Time-of-flight tip-clearance measurements

Time-of-flight tip-clearance measurements

Location Call # Status
Joyner - Microforms B300 NAS 1.15:209183 ✔ Available
Cover image for An experimental study of the effect of wake passing on turbine blade film cooling

An experimental study of the effect of wake passing on turbine blade film cooling

Location Call # Status
Joyner - Microforms B300 NAS 1.15:107425 ✔ Available
Cover image for High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction

High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction

Location Call # Status
Joyner - Microforms B300 C 13.46:1500-3 ✔ Available
Cover image for Flow conditions around the exit and downstream of certain stator blading with various trailing-edge thicknesses and geometries

Flow conditions around the exit and downstream of certain stator blading with various trailing-edge thicknesses and geometries

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Cover image for Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊

Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊

Location Call # Status
Joyner - Fed Docs Stacks ASK AT REFERENCE DESK ✔ Available
Cover image for Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊

Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊

Location Call # Status
Joyner - Fed Docs Stacks ASK AT REFERENCE DESK ✔ Available