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Cover image for Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport

Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport

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Joyner - Microforms B300 NAS 1.15:113161 ✔ Available
Cover image for Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Location Call # Status
Joyner - Microforms B300 NAS 1.15:106580 ✔ Available
Cover image for A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

Location Call # Status
Joyner - Microforms B300 NAS 1.15:106637 ✔ Available
Cover image for Engine technology challenges for a 21st century high-speed civil transport

Engine technology challenges for a 21st century high-speed civil transport

Location Call # Status
Joyner - Microforms B300 NAS 1.15:106216 ✔ Available
Cover image for Engine technology challenges for a 21st century high speed civil transport

Engine technology challenges for a 21st century high speed civil transport

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Joyner - Microforms B300 NAS 1.15:104363 ✔ Available
Cover image for NASA's program on icing research and technology

NASA's program on icing research and technology

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Joyner - Microforms B300 NAS 1.15:101989 ✔ Available
Cover image for NASA's aircraft icing analysis

NASA's aircraft icing analysis

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Joyner - Microforms B300 NAS 1.15:88791 ✔ Available
Cover image for Progress toward the development of an airfcraft icing analysis capability

Progress toward the development of an airfcraft icing analysis capability

Location Call # Status
Joyner - Microforms B300 NAS 1.15:83562 ✔ Available
Cover image for An experimental study of airfoil icing characteristics

An experimental study of airfoil icing characteristics

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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

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Joyner - Fed Docs Stacks ASK AT REFERENCE DESK ✔ Available