Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /
Charles F. Whitcomb and Harry T. Norton, Jr.
Description
| Main Author: | Whitcomb, Charles F. |
|---|---|
| Related Names: | Norton, Harry T. Jr. |
| Language(s): | English |
| Published: |
Washington, D.C. : National Advisory Committee for Aeronautics, [1956] |
| Subjects: |
Wind tunnel testing.
Leading edges (Aerodynamics) Fighter planes. Charts, diagrams, etc. Airplanes > Airplanes / Wings, Swept-back. Airplanes > Airplanes / Models > Airplanes / Models / Testing. Aerodynamics, Transonic. Charts, diagrams, etc. Wind tunnel testing. Aerodynamics, Transonic. Leading edges (Aerodynamics) Fighter planes. Airplanes > Airplanes / Models > Airplanes / Models / Testing. Airplanes > Airplanes / Wings, Swept-back. |
| Note: |
NACA Research Memorandum L55H30. On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publicatiosn Announcements No. 11. Effective Date; December 1, 1959 WHL." "March 19, 1956." Cover title. |
| Physical Description: |
30 pages :
illustrations ;
27 cm.
|
| Locate a Print Version: |
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Viewability
| Item Link | Original Source |
|---|---|
| Full view | Technical Report Archive & Image Library |