Flight Evaluation of Splitter-Plate Effectiveness in Reducing Base Drag at Mach Numbers from 0.65 to 0.90
1967
23 pages
Report
Keine Angabe
Englisch
Aerodynamics , Drag reduction , Flight test , Plate , Subsonic speed , Aircraft , Base , Blunt , Coefficient , Drag , Edge , F-104 aircraft , Flight , Hypersonic , Pressure , Reduction , Reentry , Reynolds number , Speed , Splitting , Subsonic , Test , Trailing , Vehicle