Tools
Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep / by Paul G. Fournier and B. Ann Bell.
| Main Author: | Fournier, Paul G. |
|---|---|
| Other Authors: | Bell, B. Ann. |
| Language(s): | English |
| Published: |
Washington, [D.C.] : National Aeronautics and Space Administration, 1961. |
| Subjects: |
Leading edge sweep.
Circles (Geometry) Paragliders. Pressure distribution. Planforms. Rigid wings. Transonic wind tunnels. Angle of attack. Trailing edges. |
| Note: |
Cover title. "November 1961." "Langley Research Center, Langley Air Force Base, Va." Also available from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 4/09/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980228464_1998393854.pdf. "NASA TN D-983." Document ID: 19980228464. Report Number: L-1757. |
| Physical Description: |
51 p. :
ill. ;
26 cm.
|
| Original Format: | Book |
| Locate a Print Version: |
Find in a library |
Viewability:
- Full view (original from University of Illinois)