\ud Force And Moment Measurements Were Made On 1/20th Scale Complete Model And Core Alone Of Augmented Satellite Launch Vehicle (ASLV) With Relocation O1 Secondary Injected Thrust Vector Control Tanks (SITVC Tanks) . Four Configurations Of Complete Model With 4, 6, 6M And 8 SITVC Tanks And Two Configurations Of Core Alone With 2 And 4 SITVC Tanks Were Selected For The Study . Tests Were Conducted In NAL 1 .2m Wind Tunnel At Mach Numbers 2 .1 And 2 .5 On Complete Model And On Core Alone At Mach Numbers 2 .1, 2 .5 And 3 .0 In The Incidence Range Of -6° To 6° . Significant Variations In Normal Force, Side Force, Axial Force, Pitching Moment And Yawing Moment With Relocation Of SITVC Tanks On ASLV Complete Model And Core Alone Were Observed.The...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Conventionally, launch vehicle models are mounted on sting support systems for overall force / momen...
Wind tunnel tests were conducted to study the effect of roll\ud and protuberances on the aerodynamic...
Wind Tunnel Test Results On 1/20th Scale Complete Model And Core Alone Model Of ASLV With Eight SITV...
Force measurements on a 1/35 scale model of the ASLV\ud (Augmented Satellite Launch Vehicle) have be...
Force measurements were made on one of the two boosters of the Augmented Satellite Launch Vehicle (A...
Wind tunnel studies were carried out to obtain pressure distribution in the strap-on booster interfe...
Wind tunnel tests were conducted on a 1/40 scale PSLV model to determine the aerodynamic characteri...
This report presents the results of an experimental programme for the testing of aeroelastically sca...
A 1 :20 Scale aeroelastic model of ASLV is designed for\ud studying its transonic buffet response. T...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Measurements of lift, drag and pitching moment have been made in the. No. lA Wind Tunnel at the Col...
In modern launch vehicles, the unsteady aerodynamic forces caused by flow separation during the tran...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Conventionally, launch vehicle models are mounted on sting support systems for overall force / momen...
Wind tunnel tests were conducted to study the effect of roll\ud and protuberances on the aerodynamic...
Wind Tunnel Test Results On 1/20th Scale Complete Model And Core Alone Model Of ASLV With Eight SITV...
Force measurements on a 1/35 scale model of the ASLV\ud (Augmented Satellite Launch Vehicle) have be...
Force measurements were made on one of the two boosters of the Augmented Satellite Launch Vehicle (A...
Wind tunnel studies were carried out to obtain pressure distribution in the strap-on booster interfe...
Wind tunnel tests were conducted on a 1/40 scale PSLV model to determine the aerodynamic characteri...
This report presents the results of an experimental programme for the testing of aeroelastically sca...
A 1 :20 Scale aeroelastic model of ASLV is designed for\ud studying its transonic buffet response. T...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Measurements of lift, drag and pitching moment have been made in the. No. lA Wind Tunnel at the Col...
In modern launch vehicles, the unsteady aerodynamic forces caused by flow separation during the tran...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Conventionally, launch vehicle models are mounted on sting support systems for overall force / momen...
Wind tunnel tests were conducted to study the effect of roll\ud and protuberances on the aerodynamic...