Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
19 results returnedSearch results
- Aerodynamic Investigation of a Parabolic Body of Revolution at Mach Number of 1.92 and Some Effects of an Annular Jet Exhausting From the Base
- Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel
- The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow
- A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing
- The Base Pressure at Supersonic Speeds on Two-Dimensional Airfoils and Bodies of Revolution (With and Without Fins) Having Turbulent Boundary Layers
- A summary of information on support interference at transonic and supersonic speeds
- Pressure rise associated with shock-induced boundary-layer separation
- Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams
- Investigation at supersonic speeds of external-drag effects and pumping characteristics of a short ejector
- Initial inclination of the mixing boundary separating an exhausting supersonic jet from a supersonic ambient stream
- Boundaries of Supersonic Axisymmetric Free Jets
- Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
- A rapid method for predicting attached-shock shape
- Base pressure at supersonic speeds on two-dimensional airfoils and on bodies of revolution with and without fins having turbulent boundary layers
- A reexamination of the use of simple concepts for predicting the shape and location of detached shock waves
- The Use of Cones as Stabilizing and Control Surfaces at Hypersonic Speeds
- Supersonic Wave Interference Affecting Stability
- Supersonic wave interference affecting stability
- Shape of Initial Portion of Boundary of Supersonic Axisymmetric Free Jets at Large Jet Pressure Ratios