A 0 .686-Scale Standard Dynamics Model Incorporating Some Tpecial Features Was Designed And Built At NAL .A Brief . Description Of The Various Design And Construction Features, Load Estimations And A Detailed Stress Analysis Of The Model Are Presented In The Report To Provide An Idea Of The Current Practice Adopted At NAL For The Design And Construction Of Wind Tunnel Models For Dynamic Stability Testing . The Model Was Successfully Employed For Check-Out And Validation Of A Forced-Oscillation Rig At Mach Numbers Up to 1.3 And Angles Of Attack Up to 20 Deg In The NAL 1.2m Blowdown Tunne
Several experimental databases of aeroelastic measurements performed on aircraft wing models are ava...
A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum-Tur...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
A 0 .686-Scale Standard Dynamics Model Incorporating Some Tpecial Features Was Designed And Built At...
A Proposal . Has Been Made By The Structures Division, NAL To Conduct Tests On A PRITHVI Aeroelastic...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
A 1 :20 Scale aeroelastic model of ASLV is designed for\ud studying its transonic buffet response. T...
Wind tunnel tests comprising of flow visualization and measurement of forces and moments have been ...
Wind Tunnel. Tests' Comprising Of Flow'-Visualization And Measurement - Of Forces And Moments Have B...
Abstract: The aircraft manufacturer Embraer, the German Aerospace Center (DLR), the Netherlands Aero...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Fabrication of scaled models of aircraft and other configurations for wind tunnel testing is a highl...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
A half wing model, a test rig and new wind tunnel walls were designed to study the vortex developmen...
This volume covers the phases from design to manufacturing of a wind tunnel testsupport structure fo...
Several experimental databases of aeroelastic measurements performed on aircraft wing models are ava...
A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum-Tur...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
A 0 .686-Scale Standard Dynamics Model Incorporating Some Tpecial Features Was Designed And Built At...
A Proposal . Has Been Made By The Structures Division, NAL To Conduct Tests On A PRITHVI Aeroelastic...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
A 1 :20 Scale aeroelastic model of ASLV is designed for\ud studying its transonic buffet response. T...
Wind tunnel tests comprising of flow visualization and measurement of forces and moments have been ...
Wind Tunnel. Tests' Comprising Of Flow'-Visualization And Measurement - Of Forces And Moments Have B...
Abstract: The aircraft manufacturer Embraer, the German Aerospace Center (DLR), the Netherlands Aero...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Fabrication of scaled models of aircraft and other configurations for wind tunnel testing is a highl...
A technique of testing wind-tunnel powered models has been developed as a result of experience gaine...
A half wing model, a test rig and new wind tunnel walls were designed to study the vortex developmen...
This volume covers the phases from design to manufacturing of a wind tunnel testsupport structure fo...
Several experimental databases of aeroelastic measurements performed on aircraft wing models are ava...
A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum-Tur...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...