Add to ORKGThe models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted on stings. For pressure measurements, the model is directly secured on to the sting and for force measurements, the model is supported via a balance mounted on the stings.13
In wind tunnel testing the interference of the model mount with the flow needs to be investigated. T...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
Wind tunnel model support stings can be subjected to transient aerodynamic and inertial loads which ...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Wind tunnel tests were conducted to provide sting-support interference information for planning and ...
Conventionally, launch vehicle models are mounted on sting support systems for overall force / momen...
The need to test large models at maximum speed regimes close to 100 m/s, for which the aerodynamic f...
A research program was initiated for the purpose of investigating some of the problem areas in regar...
ABSTRACT: The equipment and techniques described in detail in this report were developed especially ...
Wind tunnels are used to test scale-model air frames in order to collect aerodynamic data. The Subso...
The attached Thesis and undergraduate research are submitted to satisfy the Transcript Notation requ...
The present work is part of a broader investigation aimed at improving the understanding of the aero...
Wind tunnel tests were conducted to provide support interference information for planning and direct...
In wind tunnel testing the interference of the model mount with the flow needs to be investigated. T...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...
Wind tunnel model support stings can be subjected to transient aerodynamic and inertial loads which ...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Wind tunnel tests were conducted to provide sting-support interference information for planning and ...
Conventionally, launch vehicle models are mounted on sting support systems for overall force / momen...
The need to test large models at maximum speed regimes close to 100 m/s, for which the aerodynamic f...
A research program was initiated for the purpose of investigating some of the problem areas in regar...
ABSTRACT: The equipment and techniques described in detail in this report were developed especially ...
Wind tunnels are used to test scale-model air frames in order to collect aerodynamic data. The Subso...
The attached Thesis and undergraduate research are submitted to satisfy the Transcript Notation requ...
The present work is part of a broader investigation aimed at improving the understanding of the aero...
Wind tunnel tests were conducted to provide support interference information for planning and direct...
In wind tunnel testing the interference of the model mount with the flow needs to be investigated. T...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
This paper presents the measurement of side force, pitching, and yawing moments on a model, using an...