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Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80° delta-wing missile / by Eugene D. Schult.
| Main Author: | Schult, Eugene D. |
|---|---|
| Language(s): | English |
| Published: |
Washington, [D.C.] : National Aeronautics and Space Administration, 1960. |
| Subjects: |
Control surfaces.
Delta wings. Drag. Free flight. Jet control. Spanwise blowing. Spoilers. Zero lift. Mach number. Subsonic speed. Thrust control. Trailing edges. Wakes. Wedge flow. |
| Note: |
Title from cover. "February 1960." "Langley Research Center, Langley Field, Va." Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 1/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068625_1989068625.pdf. "NASA TN D-205." |
| Physical Description: |
47 p. :
ill. ;
26 cm.
|
| Original Format: | Book |
| Locate a Print Version: |
Find in a library |
Viewability:
- Full view (original from University of Illinois)