Free Flight Investigation At Mach Numbers Between 05 And 17 Of The Zero Lift Rolling Effectiveness And Drag Of Various Surface Spoiler And Jet Controls On An 80 Delta Wing Missile
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Index of NASA Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 500 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 860 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
Index to NASA Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 208 |
| Release | : 1959 |
| Genre | : |
| ISBN | : |
Monthly Catalog of United States Government Publications
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 2106 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
A New Dimension, Wallops Island Flight Test Range
| Author | : Joseph Adams Shortal |
| Publisher | : |
| Total Pages | : 808 |
| Release | : 1978 |
| Genre | : Aeronautics |
| ISBN | : |
Summary of Roll Controls Applicable to Fin-stabilized Vehicles
| Author | : Eugene D. Schult |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1964 |
| Genre | : Fins (Anatomy) |
| ISBN | : |
This paper discusses the rolling effectiveness of deflected fins, flaps, spoilers, and jet devices which may be employed on fin-stabilized vehicles. The possible applications and some of the significant factors affecting the performance of each device are described. The experimental information has been published previously and was obtained chiefly from free-flight tests of fin-stabilized vehicles at Mach numbers up to approximately 2.0. Comparisons are made in some cases with existing theory, which is also relied upon to indicate trends where data are not available.
