| Download | - View final version: Wind tunnel tests of a 0.04 scale model of Avro C-105 vertical tail at supersonic speeds (PDF, 27.0 MiB)
|
|---|
| DOI | Resolve DOI: https://doi.org/10.4224/40001709 |
|---|
| Creator | Search for: Conlin, L. T. |
|---|
| Format | Text, Technical Report |
|---|
| Physical description | 1 PDF/A (26 MB), 32 p. |
|---|
| Subject | Avro Arrow; Avro Canada; A.V. Roe Canada; Avro Canada CF-105 Arrow; CF-105; Canada supersonic jet; delta-winged supersonic interceptor |
|---|
| Abstract | Tests have been made in the N.A.E. 30" x 16" high speed wind tunnel on a 0.04 scale model of the vertical tail of the C-105 aircraft to determine the vertical tail load characteristics and rudder hinge moment data. The tests were made at Mach numbers 1.22, 1.35, 1.57, 1.78 and 2.03. The corresponding Reynolds number range is shown in figure 4. |
|---|
| Publication date | 1957 |
|---|
| Date distributed online | 2021-06-07 |
|---|
| Publisher | National Research Council Canada. National Aeronautical Establishment. Aerodynamics |
|---|
| Licence | |
|---|
| Access condition | - The print copies are housed in the
Rare books collection at the National Research Council of Canada. For access to print,
permission to reproduce for commercial purposes, or questions related to the collection
please contact NRC.NSL-BSN.CNRC@nrc-cnrc.gc.ca.
|
|---|
| Series | |
|---|
| Note | Distributed online by the National Research Council of Canada |
|---|
| Language | English |
|---|
| Export citation | Export as RIS |
|---|
| Collection | Avro Canada CF-105 Arrow |
|---|
| Record identifier | 787027f0-c0d6-4cc4-8eb9-329d2caa1838 |
|---|
| Record created | 2021-06-03 |
|---|
| Record modified | 2025-11-21 |
|---|
