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Flight test results of a trailing edge flap designed for direct-lift control / by Charles R. Taylor.
| Main Author: | Taylor, Charles R. |
|---|---|
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration ; 1969. |
| Subjects: |
Boundary layers.
Flight tests. Trailing-edge flaps. Aerodynamic characteristics. Deceleration. Jet impingement. Turbulent boundary layer. Airplanes > Flight testing. Trailing edge flaps. Flaps (Airplanes) |
| Note: |
"October 1969"--Cover. Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690029434%5F1969029434.pdf. "NASA CR-1426." |
| Physical Description: |
vi, 80 p. :
ill. ;
27 cm.
|
| Original Format: | Book |
| Locate a Print Version: |
Find in a library |
Viewability:
- Full view (original from University of Illinois)