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naca-tn-137

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National Advisory Committee for Aeronautics, Technical Notes - Experiments with Fabrics for Covering Airplane Wings

naca-tn-137-experiments-with-fabrics-for-covering-airplane-wings-1

The following report deals principally with the strength
and deformation of the fabric itself, both undoped and doped.
In the course of the investigations, it appeared that the
doping of the fabric with "Gallon" exercises a predominant
influence on the results, according to the nature and number
of the coats. It was decided, therefore,-to conduct the ex—
periments_in such a way that the prOperties of the fabric
when subjected to stresses would be brought out to the best
advantage. At the same time, it was endeavored to adapt the
degree of doping to actual conditions and to obtain greater
uniformity of elongation along warp and filling.

Hence two coats of cellon are applied for all comparative
tests. Parallel individual tests were also conducted with the
undoped fabric, as likewise with fabric doped three and four
times and then painted.

In a general way the figures obtained are not immediately
applicable in practice. Still less are they to be taken as
standard (with the exception of the results of individual tests
with repeated doping). By comparative tests, however, with the
usual repeated doping, individual standard figures may be ob-
* From Technische Berichte, Vol. 3, No. 3, pp, 57—73 — (1918).

tained from the experiments. These results are disregarded in
the present report, it being preferred to initiate further re-
searches with the customary doping and also with various kinds
of dope. On the other hand, the research apparatus, methods
and instructions are along the same lines as for the previous
experiments.

Wing fabrics are never used in the undoped condition, but
after being put on the ribs, are always given several coats of
dope and then painted over, if a different color is desired.
This report, therefore, deals particularly with fabric prepared
in this way, and plain fabric is considered only for the pur-
pose of comparison.

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naca-tn-137

  • Version
  • 147 Downloads
  • 2.31 MB File Size
  • 1 File Count
  • November 3, 2016 Create Date
  • November 3, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Experiments with Fabrics for Covering Airplane Wings

naca-tn-137-experiments-with-fabrics-for-covering-airplane-wings-1

The following report deals principally with the strength
and deformation of the fabric itself, both undoped and doped.
In the course of the investigations, it appeared that the
doping of the fabric with "Gallon" exercises a predominant
influence on the results, according to the nature and number
of the coats. It was decided, therefore,-to conduct the ex—
periments_in such a way that the prOperties of the fabric
when subjected to stresses would be brought out to the best
advantage. At the same time, it was endeavored to adapt the
degree of doping to actual conditions and to obtain greater
uniformity of elongation along warp and filling.

Hence two coats of cellon are applied for all comparative
tests. Parallel individual tests were also conducted with the
undoped fabric, as likewise with fabric doped three and four
times and then painted.

In a general way the figures obtained are not immediately
applicable in practice. Still less are they to be taken as
standard (with the exception of the results of individual tests
with repeated doping). By comparative tests, however, with the
usual repeated doping, individual standard figures may be ob-
* From Technische Berichte, Vol. 3, No. 3, pp, 57—73 — (1918).

tained from the experiments. These results are disregarded in
the present report, it being preferred to initiate further re-
searches with the customary doping and also with various kinds
of dope. On the other hand, the research apparatus, methods
and instructions are along the same lines as for the previous
experiments.

Wing fabrics are never used in the undoped condition, but
after being put on the ribs, are always given several coats of
dope and then painted over, if a different color is desired.
This report, therefore, deals particularly with fabric prepared
in this way, and plain fabric is considered only for the pur-
pose of comparison.

FileAction
naca-tn-137 Experiments with Fabrics for Covering Airplane Wings.pdfDownload 
17,005 Documents in our Technical Library
2727363 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...