Add to ORKGThe Supersonic tunnel located in Patterson Labs at Mississippi State University has been thoroughly documented for future reference purposes. Data acquisition, physical components, shutdown devices, a control program, and the hydraulic system are all discussed in detail. Analysis is performed showing that the flow within the Mach 2 nozzle only reaches Mach 1.8 for a portion of the flow, but that this portion of the flow is relatively stable for a wide range of settling chamber pressures. It is concluded that the tunnel with the nozzle blocks used functions correctly
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1992.Includes...
A quantitative global intensity-based temperature-sensitive paint heat-transfer measurement system h...
The objective of this thesis was to develop an experimental method to research circulation control w...
Achieving higher Mach numbers for private and commercial flight is a growing interest in the aerospa...
This document describes the design of a supersonic and a subsonic test section for a high enthalpy w...
A new 3"x3" supersonic wind tunnel was built to facilitate the continued development of localized ar...
Fluid flow and heat transfer coefficient associated with flow inside short holes (L/D=1) discharging...
This thesis documents the design, construction, and functionality of a large-scale wind tunnel desig...
An unsteady wind tunnel was designed and built for the study of unsteady aerodynamics. The wind tunn...
The next generation air breathing engine that would enable an alternative to conventional air travel...
A new transonic wind tunnel facility was designed and built on the University of Illinois at Urbana-...
Active flow control offers much promise for improved aircraft performance by delaying stall, increas...
The Lower Mississippi River Physical Model (LMRPM) is a distorted, movable-bed physical model that r...
To test shroud and blade cooling effectiveness, a closed loop, heated wind tunnel housing a film coo...
The geometry and the nature of supersonic flow in supersonic mixed compression inlets generate inter...
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1992.Includes...
A quantitative global intensity-based temperature-sensitive paint heat-transfer measurement system h...
The objective of this thesis was to develop an experimental method to research circulation control w...
Achieving higher Mach numbers for private and commercial flight is a growing interest in the aerospa...
This document describes the design of a supersonic and a subsonic test section for a high enthalpy w...
A new 3"x3" supersonic wind tunnel was built to facilitate the continued development of localized ar...
Fluid flow and heat transfer coefficient associated with flow inside short holes (L/D=1) discharging...
This thesis documents the design, construction, and functionality of a large-scale wind tunnel desig...
An unsteady wind tunnel was designed and built for the study of unsteady aerodynamics. The wind tunn...
The next generation air breathing engine that would enable an alternative to conventional air travel...
A new transonic wind tunnel facility was designed and built on the University of Illinois at Urbana-...
Active flow control offers much promise for improved aircraft performance by delaying stall, increas...
The Lower Mississippi River Physical Model (LMRPM) is a distorted, movable-bed physical model that r...
To test shroud and blade cooling effectiveness, a closed loop, heated wind tunnel housing a film coo...
The geometry and the nature of supersonic flow in supersonic mixed compression inlets generate inter...
Thesis (B.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1992.Includes...
A quantitative global intensity-based temperature-sensitive paint heat-transfer measurement system h...
The objective of this thesis was to develop an experimental method to research circulation control w...