T. O. M. Microfilm Reel 103

(Original Identification AD1(K) 48-(C-4)-Part II)

Table of Contents

Report No. E.8 M 11-11

The D.V.L single cylinder fuel test engine. August 28, 1943. Frames 7506-7520. 15 pages, pages 1-7 missing.

D.1 1 Preprints from the 1942 Year book of German Aviation research. Collection of published articles. Supply (“Liefering”) 7. Volume 10 Issue 1. January 15, 1943. Frames 7521-7603. 83 pages. Includes internal index/table of contents.

D.2 3 Preprints from the 1942 Year book of German Aviation research. Collection of published articles. Supply (“Liefering”) 8-9. Volume 10 Issue 3. March 15, 1943. Frames 7604-7731. 128 pages. Includes internal index/table of contents.

D.3 5 Preprints from the 1942 Year book of German Aviation research. Collection of published articles. Supply (“Liefering”) 1-2. Volume 9 Issue 5. October 15, 1942. Frames 7732- 7869. 140 pages. Includes internal index/table of contents.

D.4. 6 Preprints from the 1942 Year book of German Aviation research. Collection of published articles. Supply (“Liefering”) 3-4. Volume 9 Issue 6. December 1, 1942. Frames 7870-8001. 133 pages. Includes internal index/table of contents.

D.5. 7 Preprints from the 1942 Year book of German Aviation research. Collection of published articles. Supply (“Liefering”) 5-6. Volume 9 Issue 7. December 30, 1942. Frames 8002-8132. 131 pages. Includes internal index/table of contents.

D.6 12 Translations of foreign aviation literature. Volume 11 Issue 12. December 15, 1944. Frames 8133-8175. 43 pages. Includes internal index/table of contents.

The following reports/articles appear in the master (TOM reel 307) table of contents for reel 103, but were not on the microfilm reel scanned in this project. Reel 102 ends at frame 6622, and the start of reel 103 acquired here begins at frame 7506. It would appear that these reports originally consisted of these missing frames. We will attempt to ascertain whether these images are available elsewhere, but present those that are available (above) at the present time.

H15 417 Experiments with safety fuel 15.6.40

H16 418 Stroboscope for injection nozzlle investigations 26.4.40

H17 419 Test on the performance of Pump 2 in op.87 of 5.4.40 17.4.40

H18 421 Measurement of the heat conductivity of stones for

The internal insulation of high pressure ovens 27.5.40

H19 422 The measurement of cetane numbers down to zero 5.6.40

H20 424 Investigation of light firebricks “Didier Pa 08” as 18.6.40

H21 425 Lubricating oil testing with the BMW – 132 sungle

cylinder engine 25.8.40

H22 426 Ignition delay measurements with the F.K.F.S. apparatus 30.7.40

H23 427 Measuring the heat transfer of pipes with welded and

Pressed on ribs 16.7.40

H24 428 Investigation of the light firebrick “Anawerk

L.O. 9/26/2.” 1940

H25 429 Relating between cetane numbers determined with the I.G. test diesel and the H.W.A. engine 21.8.40

H26 430 Investigation of two cement asbestos compounds for

High pressure insulation 24.8.40

H28 432 Heat transfer through an incrested high pressure

pipe 13.9.40

H29 434 Collection of results on the latest investigation on

high pressure insulations 12.10.40

H30 435 New apparatus for determining knock intensity 25.10.40

H31 436 Detection of knock vibrations in multi-cylinder engines 31.10.40

H32 437 Classification standard for aviation fuels and aero

engines 5.6.40

H33 443 Measurement of performance of the pump from the turbine

aggreregate two in O.P. 87 of 31.10.40 2.12.40

H34 451 Influence of temperature on the behavior of aero

Engines operating according to the “Ring” 3.4.41

H35 459 Measurement of the performance of the pump from the

turbine aggregate 1. in Op. 87 from 5.3.41 7.5.41

H36 488 Radiation and temperature distribution in a contact

pipe of 250 mm. 29.1.42

H37 492 Results on the correlation of the Oppau method 9.10.43

E. 1 K3M2G 11 Influence of the lead content of the fuel on the

construction materials of aero engines 1.8.42

E. 2 M2K30 11 Influence of the lead content on aero engine components 23.10.42

E. 3.M2 Description of Russian Aero engines AM 35 to AM 38 1.8.42

E. 4 06K3 13 The measurement of piston temperature in an engine whilst running 20.10.42

E. 5 G 35 Experiements with the “Four Ball” machine 23.7.43

E. 6 G35 A27 Measurement of friction coefficients with the P.T.R.

apparatus 10.7.43

E. 7 G35-2 Sulphur content and lubricating properties of aero

Engines oils 25.7.43