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MECHANICS |
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TOM REEL |
BAG |
ITEM |
FRAMES |
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ADIABATIC change of state in dissociation of gases and method of sound dispersion for study of very rapid homogeneous gas reactions, by G. Damkoehler |
248 |
70 ’31-70 ‘44 |
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ANGULAR velocity |
69 |
710-711 |
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AVIATION motors, rotational vibration measurements on auxiliary drives of, (1941 Yearbook of German Aviation Study) |
94 |
71-75 |
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COMPRESSIBLE fluid, approximation method for plant potential flow of, by Wolfgang Grobner |
95 |
295-299 |
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CRANKSHAFTS, motion and free mass force of, (1941 Yearbook of German Aviation Study), by Lutz Weiler |
94 |
63-68 |
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“ , torsion of first and second kind in, (1941 Yearbook of German Aviation Study), by Kimmel |
94 |
57-63 |
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CYLINDER walls exposed to strain and interior pressure, bulging resistance of strengthened |
103-I |
7852-7857 |
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CYLINDRICAL flow, making visible |
93 |
151-155 |
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ELLIPTIC wings, six component measurements of |
103-I |
7687-7695 |
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ENGINES, rotational vibration studies in, (1941 Yearbook of German Aviation Study), by Buske |
94 |
68-71 |
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| ENSKOG principle as basis of phenomenological kinetics and its application to flames and electric gas discharges, by E. Behrens | 172 242 | 50 | 401-416 70 ’88-70 ‘111 | |
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ENTRAINMENT in tubular equipment, rate of, by A. B. Fradkov, Kislorod 1947, No. 2, pp. 16-23, in Russian |
258 |
50 ’51-50 ‘54 |
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EVALUATION in hydrodynamic processes, quantitative |
91 |
559-572 |
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FLOW resistance, influence of on fluidity of liquids of high viscosity |
107 |
29127-29134 |
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“ resistance in plane rectangular tubes with particular attention to initial losses |
103-I |
8037-8058 |
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“ through turbine blade grid, experiments on |
103-I |
8085-8093 |
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FORCES keeping airplane in straight line while rolling over ground and tendencies of side-tracking |
103-I |
8004-8017 |
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FRICTION, hydrodynamic theory of |
182 |
7084-7086 |
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FRICTIONAL losses between filter outlet and suction pipe, computation of |
91 |
646-651 |
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GEAR movement problem for artillery |
103-I |
7993-7997 |
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GYRO wing aeroplanes, influence of subsonic speeds on slide number of |
103-I |
7713-7720 |
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HYDRAULIC resistance in rectifying columns with gauze plates, by N. M. Zhavoronkov and I. E. Furner, Kislorod 1947, No. 5, pp. 9-20, in Russian |
258 |
60 ’51-60 ‘57 |
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HYDRODYNAMIC studies with ultramicroscope |
91 |
438-443 |
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HYDRODYNAMICS of foreign aviation engines |
91 |
592-632 |
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IMPULSE component of hydrodynamics |
91 |
431-437 |
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KINETIC investigation of very rapid homogeneous gas reactions, apparatus for, by Damkoehler and Sander |
172 |
108-128 |
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“ theory of flame combustion, status of, by E. Behrens |
172 |
421-439 |
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242 |
80 ‘6-80 ‘28 |
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KINETICS, structure and combustion, of diffusion flames, by E. Behrens |
172 |
417-420 |
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242 |
80 ‘1-80 ‘5 |
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LAMINATED friction layer, unstable disturbances in |
103-I |
7568-7585 |
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LATERAL stability for aircrafts, calculations of |
103-I |
7696-7703 |
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LAVAL nozzle, current field of |
103-I |
7774-7785 |
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MIDDLE wing aeroplane, investigation on distribution of pressure near main wing connection of |
103-I |
7676-7681 |
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MOMENT of inertia around transverse axis of large aeroplanes, experimental determination of |
103-I |
7740-7745 |
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NOZZLE influence on wind tunnel corrections in steady air current |
103-I |
7595-7602 |
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PROPELLER blades, construction of |
103-I |
7745-7758 |
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“ blades, relation of shape of to strain by centrifugal forces |
103-I |
73907930-7931 |
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PROPELLERS, investigation of vibrations of counterwise rotating |
103-I |
7896 |
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REACTION kinetics of oxidation of n- and i-paraffins, investigation on, by L. v. Mueffling |
248 |
70 ’14-70 ‘23 |
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RECOIL forces caused by discharge of gases or liquids from broken high pressure lines, determination of by Grader |
174 |
513-534 |
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ROTATING swinging systems, investigations, measurements and tests of centrifugal pendulums in |
103-I |
7638-7652 |
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SHEARING strength of some wooden aircraft construction materials, comparative |
103-I |
8163 |
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STABILITY limits of circular cylinder walls |
103-I |
7806-7820 |
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“ conditions in Fieseler shaft towing aircraft |
103-I |
7721-7730 |
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STRESS, additional in steel-duraluminum constructions caused by heat expansion |
103-I |
8018-8023 |
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STROBOSCOPE for nozzle research, by Schuch |
103-II |
3 |
7060-7075 |
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Translation |
244 |
20 ‘90 |
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THREE membered joints, computation of compression of (1941 Yearbook of German Aviation Study) Risan |
94 |
91-93 |
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TURBINES with axial flow (1941 Yearbook of German Aviation Study), by Weinig |
94 |
101-104 |
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VARYING density of flowing media with horizontal movement components, effect of on course of flow |
174 |
657-658 |
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VERY rapid homogenous gas reactions, isentropic changes in state of dissociating gases and methods of sound propagation for study of, (1942 Year-book of German Aviation Study) |
94 |
438-448 |
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WEIGHT distribution across entire wing span |
103-I |
7612-7619 |