Browse TRAIL Inventories

Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9

Flow separation ahead of a blunt axially symmetric body at Mach numbers 1.76 to 2.10

Preliminary investigation of use of conical flow separation for efficient supersonic diffusion

Interaction of oblique shock waves with regions of variable pressure, entropy, and energy

Use of aerodynamic heating to provide thrust by vaporization of surface coolants

Estimation of inlet lip forces at subsonic and supersonic speeds

Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds

Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds

Oblique-shock relations at hypersonic speeds for air in chemical equilibrium

Composition and thermodynamic properties of air in chemical equilibrium


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