Identifier
|
Title
|
Level of description
|
Date
|
Digital object |
|
|
2 |
'Wind Tunnel Measurements of the Hinge Moments on Bomb Doors beneath an Engine Nacelle'. Division of Aeronautics, Report No A3 by T F C Laurence and G K Batchelor |
Item |
Jan 1941 |
|
|
|
4 |
'Sighting Corrections for a Free Gun'. Division of Aeronautics Report, No A4 Addendum by G K Batchelor |
Item |
May 1941 |
|
|
|
11 |
'Ducted Cooling Tests Comparing the Normal Ring-Gill Exit with a Flap-Exit beneath the Wing'. Division of Aeronautics, Report No A10 by G K Batchelor |
Item |
May 1942 |
|
|
|
12 |
"Velocity and Total Head Traverse of the Working Section of the 9’ x 7' Wind Tunnel". Division of Aeronautics, Note No A11 by G K Batchelor |
Item |
May 1942 |
|
|
|
20 |
'Determination of the Lift of an Aerofoil in a Wind Tunnel from the Pressure on the Walls'. Division of Aeronautics, Report No A24 by G K Batchelor |
Item |
Jun 1944 |
|
|
|
21 |
'A Numerical Method of Determining Subsonic Compressible Flow Past an Obstacle. II Joukowski Aerofoil'. Division of Aeronautics, Aerodynamics Note No 61 by G K Batchelor |
Item |
Dec 1944 |
|
|
|
1 |
‘Interesting documents from CSIR [Council for Scientific and Industrial Research] period’ including memoranda on the work of the Fluid Motion Group with plans for a proposed fluid motion laboratory |
Item |
1940-1944 |
|
|
|
3 |
'Sighting Corrections for a Free Gun'. Division of Aeronautics Report, No A4 by G K Batchelor |
Item |
Feb 1941 |
|
|
|
6 |
'Note on the Aerial Flight of a Torpedo Bomb'. Division of Aeronautics, Aerodynamics Note No 16 by G K Batchelor |
Item |
|
|
|
|
10 |
'Velocity and Total Head Traverse of the Working Section of the 9’ x 7’ Wind Tunnel'. Division of Aeronautics, Report No A6 by G K Batchelor |
Item |
Feb 1942 |
|
|
|
13 |
'Wind Tunnel Tests on the CA-12 Interceptor Part I: Miscellaneous Investigations'. Division of Aeronautics, Report No A11 by G K Batchelor |
Item |
Jun 1942 |
|
|
|
15 |
'Wind Tunnel Investigation on the Design of a Replacement Beaufort. Part I – Drag and Yawing Moment Measurements with New Turrets'. Division of Aeronautics, Report No A12 by P T C Lawrence and G K Batchelor |
Item |
Dec 1942 |
|
|
|
16 |
'Further Considerations of Sighting Corrections for a Free Gun – Parallel Motion Case'. Division of Aeronautics, second addendum to report A4 by G K Batchelor |
Item |
Mar 1943 |
|
|
|
17 |
'The Laminar Flow Characteristics of Three Related Aerofoils'. Division of Aeronautics, Report No A20 by G K Batchelor |
Item |
Dec 1943 |
|
|
|
8 |
'Resume of Research on Laminar Flow Shapes'. Division of Aeronautics, Aerodynamics Note No 21 by GKB |
Item |
Jan 1942 |
|
|
|
19 |
'A Numerical Method of Determining Subsonic Compressible Flow Past and Obstacle. I – Circular Cylinder'. Division of Aeronautics, Report No A11 and SM28 by G K Batchelor and F S Shaw |
Item |
Feb 1944 |
|
|
|
22 |
'Singing Corner Vanes: A Note on the Peculiar Double Resonant Sustained Oscillation Occurring in a Wind Tunnel'. Division of Aeronautics, Aeronautics Note No 62 by G K Batchelor and A A Townsend |
Item |
Jan 1945 |
|
|
|
5 |
'Note on the Resistance of Wire Gauze'. Division of Aeronautics, Aerodynamics Note No 1 by G K Batchelor |
Item |
May 1941 |
|
|
|
7 |
'Calibration of Multitube Manometer'. Division of Aeronautics, Aerodynamics Note No 5 by G K Batchelor |
Item |
Jan 1942 |
|
|
|
9 |
'Calibration and the Use of the Tunnel Speed Indicator'. Division of Aeronautics, Aerodynamics Note No 7 by GKB and J B Willis |
Item |
Feb 1942 |
|
|
|
14 |
'Note on Critical Speeds of the CA-12 Interceptor'. Division of Aeronautics, Aerodynamics Note No A15 by G K Batchelor |
Item |
1942 |
|
|
|
18 |
'Interference in a Wind Tunnel of Octagonal Section'. Australian Council for Aeronautics report ACA-1 |
Item |
Jan 1944 |
|
|
|
23 |
'Note on the Effect of Rivets and Joints on the Drag of the “Bristol Beaufort”'. Division of Aeronautics, Aerodynamics Note No 3 by G K Batchelor |
Item |
n.d. |
|
|
|
24 |
'Calibration of Pitot-Static Tubes'. Division of Aeronautics, Aerodynamics Note No 61 by G K Batchelor |
Item |
n.d. |
|
|
