Catalog Search Results
Author
Series
NASA technical paper volume X-52374
Publisher
National Aeronautics and Space Administration
Pub. Date
[November 1967]
Language
English
Formats
Author
Series
NASA technical paper volume 1108
Publisher
National Aeronoautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1066
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Description
The optical performance of a virtual image display system is evaluated. Observation of a two-element (unachromatized doublet) refractive system led to the conclusion that the major source of image degradation was lateral chromatic aberration.
Author
Series
NASA technical paper volume 1032
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1018
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1070
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1016
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1074
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1071
Publisher
National Aeronautics and Space Administration
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1050
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1057
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1079
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1054
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
September 1977.
Language
English
Formats
Author
Series
NASA technical paper volume 1058
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
September 1977.
Language
English
Formats
Author
Series
NASA technical paper volume 1093
Publisher
National Aeronautics and Space Administration
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1096
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Description
Sliding friction experiments were conducted with 1045 steel contacting 302 stainless steel and lubricated with various organometallics in mineral oil. Auger emission spectroscopy was used to determine the element present in the wear contact zone. The results indicate that there are organometallics which are as effective an antiwear additives as the commonly used zinc dialkyl dithiophosphate. These include dimethyl cadmium, triphenyl lead thiomethoxide,...
Author
Series
NASA technical paper volume 1063
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Author
Series
NASA technical paper volume 1090
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office
Pub. Date
1977
Language
English
Formats
Description
The effects of power on the longitudinal aerodynamic characteristics of a close-coupled wing-canard fighter configuration with partial-span rectangular nozzles at the trailing edge of the wing were investigated. Data were obtained on a basic wing-strake configuration for nozzle and flap deflections from 0 deg to 30 deg and for nominal thrust coefficients from 0 to 0.30. The model was tested over an angle-of-attack range from -2 deg to 40 deg at Mach...
Author
Series
NASA technical paper volume 1095
Publisher
For sale by the National Technical Information Service
Pub. Date
1977
Language
English