An investigation of 0.15-chord ailerons on a low-drag tapered wing at high speeds / by Edmund V. Laitone.
Tests of 0.15-wing-chord, internally balanced ailerons on a low-drag tapered wing were made at Mach numbers up to 0.75. The corresponding Reynolds number range was from 5,000,000 to 13,800,000. Both a normal-profile and a beveled, trailing-edge aileron were tested without a seal and with a partial s...
Saved in:
| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series A. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. A24. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/A24
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| Y 3.N 21/5:11/A24 | Available Place a Hold |