Tools
Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight / by William A. Newsom, Jr.
| Main Author: | Newsom, William A. |
|---|---|
| Language(s): | English |
| Published: |
Washington, [D.C.] : National Aeronautics and Space Administration, 1959. |
| Subjects: |
Externally blown flaps.
Fighter aircraft. Low speed. Wind tunnel models. Wind tunnel tests. Aerodynamic characteristics. Aerodynamic forces. Augmentation flaps (control surfaces) |
| Note: |
Title from cover. "September 1959." "Langley Research Center, Langley Field, Va." Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/17/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068069_1989068069.pdf. "NASA TN D-50." |
| Physical Description: |
84 p. :
ill. ;
26 cm.
|
| Original Format: | Book |
| Locate a Print Version: |
Find in a library |
Viewability:
- Full view (original from University of Illinois)