Results of the wind tunnel tests conducted on BAe R-80 model\ud are presented in this report. The objective of the testing\ud was to compare the results obtained from facilities at NAL,\ud Bangalore and Wart on, U.K. The tests were conducted in\ud the Mach Numbers range of -5 to 20 deg in general. In general\ud the Results obtained from the facilities at NAL and Warton\ud agree well except at high incidence
The article summarises evaluation experiments in new MP1 test section suited for airfoils and bodies...
Wind tunnel tests were conducted on a 1/40 scale PSLV model to determine the aerodynamic characteri...
Results are presented of a wind tunnel investigation of a 0.1-scale model of the left-hand dual inle...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
Tests were conducted in the AEDC Propulsion Wind Tunnel (16T) to determine the tunnel test section M...
Wind tunnel tests comprising of flow visualization and measurement of forces and moments have been ...
The shakedown and calibrated characteristics of the new AEDC Mach Number 4 Aerothermal Wind Tunnel w...
Fabrication of scaled models of aircraft and other configurations for wind tunnel testing is a highl...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
A new research scheme for a full-scale/model test comparison is proposed for effectively validating ...
An Indigenous Flying Helmet Was Tested In The 1 .2m Wind Tunnel To Study The Effects Of Wind Blast A...
Results are presented of a wind tunnel investigation of a 0.2-scale model of the left-hand dual-inle...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Wind Tunnel. Tests' Comprising Of Flow'-Visualization And Measurement - Of Forces And Moments Have B...
The article summarises evaluation experiments in new MP1 test section suited for airfoils and bodies...
Wind tunnel tests were conducted on a 1/40 scale PSLV model to determine the aerodynamic characteri...
Results are presented of a wind tunnel investigation of a 0.1-scale model of the left-hand dual inle...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establ...
Tests were conducted in the AEDC Propulsion Wind Tunnel (16T) to determine the tunnel test section M...
Wind tunnel tests comprising of flow visualization and measurement of forces and moments have been ...
The shakedown and calibrated characteristics of the new AEDC Mach Number 4 Aerothermal Wind Tunnel w...
Fabrication of scaled models of aircraft and other configurations for wind tunnel testing is a highl...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
A new research scheme for a full-scale/model test comparison is proposed for effectively validating ...
An Indigenous Flying Helmet Was Tested In The 1 .2m Wind Tunnel To Study The Effects Of Wind Blast A...
Results are presented of a wind tunnel investigation of a 0.2-scale model of the left-hand dual-inle...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Wind Tunnel. Tests' Comprising Of Flow'-Visualization And Measurement - Of Forces And Moments Have B...
The article summarises evaluation experiments in new MP1 test section suited for airfoils and bodies...
Wind tunnel tests were conducted on a 1/40 scale PSLV model to determine the aerodynamic characteri...
Results are presented of a wind tunnel investigation of a 0.1-scale model of the left-hand dual inle...