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Cover image for Measurement uncertainty for the uniform engine testing program conducted at the NASA Lewis Research Center

Measurement uncertainty for the uniform engine testing program conducted at the NASA Lewis Research Center

Joyner Library - Microforms B300
Call Number: NAS 1.15:88943
Cover image for Small, low-cost, expendable turbojet engine

Small, low-cost, expendable turbojet engine

Joyner Library - Fed Docs Stacks
Call Number: ASK AT REFERENCE DESK
Cover image for Water ingestion testing for turbine powered airplanes

Water ingestion testing for turbine powered airplanes

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Cover image for Evaluating turbine engine operating characteristics

Evaluating turbine engine operating characteristics

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Cover image for Qualification testing of turbojet engine thrust reversers

Qualification testing of turbojet engine thrust reversers

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Cover image for Aerodynamic performance of 0.4066-scale model of JT8D refan stage

Aerodynamic performance of 0.4066-scale model of JT8D refan stage

Joyner Library - Fed Docs Stacks
Call Number: ASK AT REFERENCE DESK
Cover image for Incidence angle bounds for lip flow separation of the 13.97-centimeter-diameter inlets

Incidence angle bounds for lip flow separation of the 13.97-centimeter-diameter inlets

Joyner Library - Fed Docs Stacks
Call Number: ASK AT REFERENCE DESK
Cover image for Computer program for estimating performance of air-breathing aircraft engines

Computer program for estimating performance of air-breathing aircraft engines

Joyner Library - Microforms B300
Call Number: NAS 1.15:4254
Cover image for Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel

Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel

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Cover image for Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction

Boundary-layer bleed system study for a full-scale, mixed-compression inlet with 45 percent internal contraction

Joyner Library - Fed Docs Stacks
Call Number: ASK AT REFERENCE DESK