Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678.231F(AD-A--242-212)(microfiche) / BLDSC - British Library Document Supply CentreSIGLEGBUnited Kingdo
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX182385 / BLDSC - British Library D...
The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...
SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...
8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9002) / BLDSC - Brit...
8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...
SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...
7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8421) / BLDSC - British ...
SIGLEAvailable from British Library Document Supply Centre-DSC:D195704 / BLDSC - British Library Doc...
The study focuses on the effects of the leading-edge radius on the flow over 50º swept delta wing mo...
Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...
SIGLEAvailable from British Library Document Supply Centre-DSC:DX193620 / BLDSC - British Library Do...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN041355 / BLDSC - British Library D...
"The views expressed herein are those of the authors alone and do not necessarily represent tho...
Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX182385 / BLDSC - British Library D...
The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...
SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...
8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9002) / BLDSC - Brit...
8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...
SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9611) / BLDSC - British Libr...
7.50SIGLEAvailable from British Library Document Supply Centre- DSC:3310.76(8421) / BLDSC - British ...
SIGLEAvailable from British Library Document Supply Centre-DSC:D195704 / BLDSC - British Library Doc...
The study focuses on the effects of the leading-edge radius on the flow over 50º swept delta wing mo...
Available from British Library Document Supply Centre-DSC:DXN049905 / BLDSC - British Library Docume...
SIGLEAvailable from British Library Document Supply Centre-DSC:DX193620 / BLDSC - British Library Do...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN041355 / BLDSC - British Library D...
"The views expressed herein are those of the authors alone and do not necessarily represent tho...
Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...
Wind tunnel experiments were conducted in order to investigate the effectiveness of flow control dev...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX182385 / BLDSC - British Library D...
The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...