Add to ORKGThe goal of this project was to design and construct a small-scale, supersonic wind tunnel. The wind tunnel was intended to use the difference between atmospheric pressure and the pressure inside the vacuum chamber in WPI\u27s Vacuum Test Facility (VTF) to achieve its desired flow velocities. A previous MQP already designed a small, supersonic wind tunnel, but it was designed for one specific Mach number. As such, it was decided that this project would aim to make a tunnel capable of achieving various test section Mach numbers. The completed wind tunnel was designed for educational and research purposes
This paper describes the requirements, design, and prototype testing of the flex-section and hinge s...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
This book is intended to be a valuable addition to students, engineers, scientists, industrialists, ...
Historically, the endeavor of scale testing flight vehicles at supersonic Mach numbers, especially f...
The goal of this project was to design, construct, and conduct preliminary testing of a supersonic w...
A subsonic wind tunnel was designed and built for the University of Texas at Tyler laboratories as a...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
The purpose of this project is to design and build a wind tunnel for research and educational use in...
The research work of this thesis was part of the low-boom supersonic inlet project conducted by NASA...
The purpose of this project is to design and build a wind tunnel for research and educational use in...
Aspects of the design and construction of the Laminar Flow Supersonic Wind Tunnel at the NASA-Ames F...
A mobile and affordable, miniature wind tunnel to aid students in studying high-speed compressible f...
Hypersonics sits atop a short list of Department of Defense research priorities outlined by the 2018...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
This paper describes the requirements, design, and prototype testing of the flex-section and hinge s...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
This book is intended to be a valuable addition to students, engineers, scientists, industrialists, ...
Historically, the endeavor of scale testing flight vehicles at supersonic Mach numbers, especially f...
The goal of this project was to design, construct, and conduct preliminary testing of a supersonic w...
A subsonic wind tunnel was designed and built for the University of Texas at Tyler laboratories as a...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
The purpose of this project is to design and build a wind tunnel for research and educational use in...
The research work of this thesis was part of the low-boom supersonic inlet project conducted by NASA...
The purpose of this project is to design and build a wind tunnel for research and educational use in...
Aspects of the design and construction of the Laminar Flow Supersonic Wind Tunnel at the NASA-Ames F...
A mobile and affordable, miniature wind tunnel to aid students in studying high-speed compressible f...
Hypersonics sits atop a short list of Department of Defense research priorities outlined by the 2018...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
This paper describes the requirements, design, and prototype testing of the flex-section and hinge s...
The interaction with the planetary atmosphere is an unavoidable fact when dealing with problems rela...
This book is intended to be a valuable addition to students, engineers, scientists, industrialists, ...