Force measurements were made on one of the two boosters of the Augmented Satellite Launch Vehicle (ASLV) model, at Mach numbers 0 .8, 1 .0 and 2 .1 at angles of incidence in the range -6 to 6 degrees in the N .A .L 1 .2M Trisonic Wind Tunnel . These measurements were made to supplement the force and pressure measurements made earlier on the same configuration . Hesults of the tests are given in this document
The report presents a description of the wind tunnel tests conducted on a 0 .031 scale model of ASLV...
Unsteady pressure measurements were carried out, on the scaled configurations of Augmented Satellite...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
Force measurements on a 1/35 scale model of the ASLV\ud (Augmented Satellite Launch Vehicle) have be...
Wind Tunnel Test Results On 1/20th Scale Complete Model And Core Alone Model Of ASLV With Eight SITV...
\ud Force And Moment Measurements Were Made On 1/20th Scale Complete Model And Core Alone Of Augment...
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...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Wind tunnel tests were conducted to study the effect of roll\ud and protuberances on the aerodynamic...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
Wind tunnel studies were carried out to obtain surface pressure distribution in the strap-on booster...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
The accurate landing of entry capsules on other planets and moons depends on accurate knowledge of t...
The report presents a description of the wind tunnel tests conducted on a 0 .031 scale model of ASLV...
Unsteady pressure measurements were carried out, on the scaled configurations of Augmented Satellite...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
Force measurements on a 1/35 scale model of the ASLV\ud (Augmented Satellite Launch Vehicle) have be...
Wind Tunnel Test Results On 1/20th Scale Complete Model And Core Alone Model Of ASLV With Eight SITV...
\ud Force And Moment Measurements Were Made On 1/20th Scale Complete Model And Core Alone Of Augment...
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...
Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...
Wind tunnel tests were conducted to study the effect of roll\ud and protuberances on the aerodynamic...
An experimental Aerodynamic and Aero-Acoustic loads data base was obtained at transonic Mach numbers...
Wind tunnel studies were carried out to obtain surface pressure distribution in the strap-on booster...
A 1:20 Scale Aeroelastic model of ASLV is designed for studying its transonic buffet response.The mo...
The accurate landing of entry capsules on other planets and moons depends on accurate knowledge of t...
The report presents a description of the wind tunnel tests conducted on a 0 .031 scale model of ASLV...
Unsteady pressure measurements were carried out, on the scaled configurations of Augmented Satellite...
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...