Browse TRAIL Inventories

Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) : body of revolution with near-parabolic forebody and cylindrical afterbody

Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) II : aerodynamic load distributions of series of five bodies having conical noses and cylindrical afterbodies

Theoretical pressure distribution and wave drags for conical boattails

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) III : boundary layer and force measurements on a slender cone-cylinder body of revolution

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) IV : aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies

Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12

Variation of boundary-layer transition with heat transfer on two bodies of revolution at a Mach number of 3.12

Heat-transfer measurements on two bodies of revolution at a Mach number of 3.12

Effects of extreme surface cooling on boundary-layer transition

Boundary-layer transition at Mach 3.12 as affected by cooling and nose blunting

Effect of favorable pressure gradients on transition for several bodies of revolution at Mach 3.12


Published Year

Author