NASA Technical Reports Server (NASA) · 1979 · 20 citations · 0 references
EngineeringAerospace EngineeringAerodynamicsAircraft DesignSurface EngineeringAirfoil TheoryAttack Surface AnalysisExperimental AerodynamicsSubsonic AerodynamicsSupersonic AerodynamicsAngle Of AttackAngle Of Attack MeasurementMach NumberMach Number EffectsReynolds NumberReynolds Number EffectsSurface PressureSurface Pressure Analysis
Tabulated surface pressure data for a series of forebodies which have analytically defined cross sections and are based on a 20 degs half-angle cone are presented without analysis. Five of the cross sections were ellipses having axis ratios of 3/1, 2/1, 1/1, 1/2, and 1/3. The sixth cross section was defined by a curve having a single lobe. The data generally cover angles of attack from -5 degs to 20 degs at angles of sideslip from 0 degs to 5 degs for Mach numbers of 1.70, 2.50, 3.95, and 4.50 at a constant Reynolds number.