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Viewing 169981 to 170010 of 175570
1948-01-01
Technical Paper
480062
Fayette Leister
1948-01-01
Technical Paper
480114
H. W. BARTH, F. A. ROBBINS, H. C. LAFFERTY
1948-01-01
Technical Paper
480115
H. T. MUELLER, K. L. PFUNDSTEIN
1948-01-01
Technical Paper
480116
R. M. SCHAEFER
1948-01-01
Technical Paper
480117
J. J. BROEZE, C. STILLEBROER
1948-01-01
Technical Paper
480118
D. K. HEIPLE
1948-01-01
Technical Paper
480119
LOREN E. LURA
1948-01-01
Technical Paper
480120
C. G. A. ROSEN
1948-01-01
Technical Paper
480121
A. T. COLWELL
1948-01-01
Technical Paper
480106
ROBERT R. HOUSTON, JOHN M. PARKER
1948-01-01
Technical Paper
480107
W. B. BASSETT
1948-01-01
Technical Paper
480108
RALPH K. SUPER
1948-01-01
Technical Paper
480109
WALTER C. HADLEY, J. R. HUDNALL, A. E. TRAVER
1948-01-01
Technical Paper
480110
HANS BOHUSLAV
1948-01-01
Technical Paper
480111
L. A. BLANC
1948-01-01
Technical Paper
480099
E. S. LAND (RET.)
1948-01-01
Technical Paper
480113
O. D. TREIBER
1948-01-01
Technical Paper
480098
JOHN S. WORLEY
1948-01-01
Technical Paper
480101
JAMES T. SHORE
1948-01-01
Technical Paper
480103
R. A. Coit, L. M. Whitney, F. G. Bollo, A. G. Cattaneo
Summary The present rapid increase in the number of light aircraft and private pilots will undoubtedly lead to a more general use of these aircraft. This will also mean more frequent operation under extremes of weather and operating conditions, and will increase the tendency on the part of many users to utilize automotive rather than aviation gasoline as an engine fuel because of its wider availability. Both these factors bring the problem of fuel vapor lock closer, hence it became desirable to study light aircraft fuel systems from the standpoint of vapor handling capacity. The vapor lock limits of a typical fuel system are presented, and an analysis is made of the factors which control vapor formation and the vapor handling capacity of the system. The limits found indicate that present 7 psi. Reid vapor pressure aviation fuels can be safely used under all practical conditions in a properly designed gravity feed fuel system but diaphragm fuel pump systems are marginal.
1948-01-01
Technical Paper
480102
TED V. RODGERS
1948-01-01
Technical Paper
480105
A. H. DEIMEL
1948-01-01
Technical Paper
480091
J. W. BARRIGER
1948-01-01
Technical Paper
480104
LLYOD E. MULLER
1948-01-01
Technical Paper
480090
EARL L. MONSON
1948-01-01
Technical Paper
480093
C. R. LEWIS
1948-01-01
Technical Paper
480095
D. M. McCUTCHEON

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