Results of static tests on standard airplane tires and wheels (material section report)
| Metadata Field | Value | Language |
|---|---|---|
| dc.creator | United States. Army. Air Service. Engineering Division. | en_US |
| dc.date.accessioned | 2018-07-31T14:06:15Z | |
| dc.date.available | 2018-07-31T14:06:15Z | |
| dc.date.created | 1921-04-30 | en_US |
| dc.identifier.uri | http://hdl.handle.net/11200/49187 | |
| dc.description | The purpose of this investigation is to obtain comprehensive data on the performance of the standard sizes of airplane tires and wheels in the clincher types, and the existing straight side types size, with special reference to the load-deflection curves of the tires and ultimate strength of the various sizes of wheels. From the curves obtained in the foregoing tests, it is possible to determine the size of the wheel, size of tire, and the most satisfactory air pressure to use for any particular airplane when the weight is known. In addition, the factor of safety can be calculated from the information relative to the breaking load of wheels of various sizes. | en_US |
| dc.format | en_US | |
| dc.publisher | Washington, D.C. : Chief of Air Service | en_US |
| dc.relation.ispartofseries | Air Service information circular (Aviation) ; v. 3, no. 270 | en_US |
| dc.relation.ispartofseries | McCook Field report ; Serial no. 1496 | en_US |
| dc.subject | Wheels | en_US |
| dc.subject | Tires | en_US |
| dc.subject | Airplanes--Parts--Testing | en_US |
| dc.subject | Airplanes--Design and construction | en_US |
| dc.subject | Aeronautics--Systems engineering | en_US |
| dc.subject | Airplanes--Tires | en_US |
| dc.subject | Airplanes--Landing gear | en_US |
| dc.title | Results of static tests on standard airplane tires and wheels (material section report) | en_US |
| dc.type | Text | en_US |
Files in this item
This item appears in the following Collection(s)
- Air Service Information CircularsAir Service Information Circulars