[go: up one dir, main page]

BENEK et al., 1973 - Google Patents

A method for the prediction of the effects of free-stream disturbances on bondary-layer transition[Final Report, Jan. 1972- Mar. 1973]

BENEK et al., 1973

Document ID
13467935441958035783
Author
BENEK J
HIGH M
Publication year

External Links

Continue reading at scholar.google.com (other versions)

Similar Documents

Publication Publication Date Title
Gursul Unsteady flow phenomena over delta wings at high angle of attack
BENEK et al. A method for the prediction of the effects of free-stream disturbances on bondary-layer transition[Final Report, Jan. 1972- Mar. 1973]
Mateer The effect of angle of attack on boundary-layer transition on cones
Barnea et al. Stability of annular flow
ADAMS Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers[Final Report, Dec. 1972- Jul. 1973]
STRACH The pressure on a circular cylinder at Re= 52, 000 to Re= 186, 000 and variable Mach number(Pressure distribution and boundary layer separation measurement on circular cylinder at critical subsonic velocities for various Reynolds and Mach numbers)
Thomas The estimation of lateral-directional aerodynamic derivatives at subsonic speeds
BELOV et al. Flow at the stagnation point of an obstacle situated in plane subsonic jet flow
GREEN On the influence of free-stream turbulence on a turbulent boundary layer, as it relates to wind tunnel testing at subsonic speeds(Influence of free stream turbulence on turbulent boundary layer in relation to wind tunnel testing at subsonic speeds)
Haines Further evidence and thoughts on scale effects at high subsonic speeds
GEORGE-FALVY Scale effect studies of airfoil profile drag at high subsonic speed(Airfoil profile drag measurements, correlating full scale flight tests and scale model tests in transonic and high Reynolds number wind tunnels)
Maddalon et al. Hypersonic transition studies on a slender cone at small angles of attack.
NEHRING A kinematic approach to unsteady viscous flows
Dodge A transonic relaxation method for cascade flow systems
GARTSHORE Self-preserving flows(Structural analysis on self-preserving turbulent shear flow)
STOCK Interaction between a high speed boundary layer flow and an inelastic deformable solid wall(Interaction between supersonic boundary layer with turbulent flow and inelastic deformable wall to determine stress perturbations and pressure distribution)
FINKE Unsteady interaction between shock and detached boundary layer in a transonic flow
Lipatov Flow in the neighborhood of the point of origin of intense suction of a laminar boundary layer in supersonic flow
MILLER A method for determining the critical pressure ratio of a group of turbine stages
Landers et al. Store separation from aircraft using a captive trajectory yawmeter system
YI Incompressible turbulent separation from an axisymmetric curved afterbody(Separation of incompressible boundary layer from axisymmetric curved afterbody)[Ph. D. Thesis]
Minailos Regimes of supersonic flow past thin wings
Dyment et al. Example of aerodynamic instability under supercritical conditions about profiles
Ronald D Evolution of Stationary Crossflow Vortices in Boundary Layers on Swept Wings
JAARSMA Inlets-airplane testing in transonic wind tunnels(Data and recommendations for transonic tests of inlets)