AERODYNAMICS |
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TOM REEL |
BAG |
ITEM |
FRAMES |
|
AIR academy archives, report of |
221 |
60 ’37-60 ‘52 |
||
AIRLFLOW around rotating elipsoid, compressible, according to method of Genzen-Rayleigh |
103-I |
7954-7961 |
||
AERODYNAMIC pressure and measurements of slope of wing lift in aeroplane wing ends |
94 |
607-611 |
||
“ problems of aeroplane body |
103-I |
7710-7714 |
||
“ shaping of aviation engine housing, by T. Zobel |
221 |
70 ‘6 |
||
BOUNDARIES, laminar, in parallel flow along planes of plate by transporting mass in normal direction to plate, by G. Damkoehler |
172 |
103-107 |
||
BUOYANCY (lift) |
103-I |
8155-8162 |
||
“ (lift) of wing in inhomogeneous air current, investigations on |
103-I |
7962-7967 |
||
COMPRESSION shocks, diagram for computation of, (1941 Yearbook of German Aviation Study), by Strouse and Voigt |
94 |
39-43 |
||
EXPANSION flow in rectangular hollow space, two-dimensional |
124 |
1051-1053 |
||
FLAME experiments in tubes, aerodynamic contributions to evaluation of, by Damkoehler and Schmidt |
172 |
129-149 |
||
“ velocity in gas mixtures, effect of turbulence on, by G. Damkoehler |
172 |
150-168 |
||
FREE moment balance for measuring forces of air currents |
103-I |
7628-7632 |
||
GAS, exhaust, shocks under altitude conditions, tests on, (1941 Yearbook of German Aviation Study), Oestrich |
94 |
51-53 |
||
INERTIA of gases during firing of guns, influence of |
103-I |
8123-8131 |
||
MOTION of plate entering flow of air current, investigation of |
103-I |
7902 |
||
OPTICAL methods for measuring flow, progress in, by T. Zobel |
221 |
70 ’42-70 ‘63 |
||
PRESSURE distribution for aerodynamic profiles, calculation of |
103-I |
7535-7542 |
||
PRESIDENTIAL address at meeting of Acad. of Aviation Studies, April 1943 |
221 |
70 ‘1-70 ‘2 |
||
“ address on Germ. Acad. for Aviation Studies for 1943-1944
|
221 | 60 ’84-60 ‘99 | ||
REACTION products of gasoline-air mixture rapidly compressed in motor but not ignited, by Damkoehler and Eggersgluss |
172 |
169-198 |
||
RESEARCH, organization of aviation |
211 |
10 ’69-10 ‘72 |
||
RUDDERS, wind tunnel investigation of |
103-I |
7968-7971 |
||
STREAMS of supersonic speed hitting against conical bodies |
103-I |
8059-8069 |
||
TIPOVER point and suction |
103-I |
7799-7805 |
||
TURBULENT flow processes, quantitative evaluation with aid of slow motion pictures of |
102 |
6062-6075 |
||
VIBRATIONS, orbital, in gliders, investigation of |
103-I |
8113-8122 |
||
WHIRL trails of aircrafts, photography of |
103-I |
7998-8000 |
||
WIND current behind aircraft wing |
103-I |
7894-7895 |
||
“ flume experiments on atmospheric resistance of railway vehicles (in English) |
91 |
400-418 |
||
“ tunnels in Roumania, by Valcovici and I. Stroescu |
221 |
30 ‘121-30 ‘126 |
||
“ tunnel tests on air cooled power plants (1942 Yearbook of German Aviation Study) |
94 |
344-345 |
||
WING profiles exhibiting singularity, curves of aircraft |
103-I |
7822-7826 |