Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow I : Symmetric Flows Obeying the Simplified Density-speed Relation
Explore the source record for details and available documents.
Bers, Lipman↗
SEARCH · Search NASA
Results for “VELOCITY DISTRIBUTION”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Velocity distribution on wing sections of arbitrary shape in compressible potential flow II : subsonic symmetric adiabatic flows
Explore the source record for details and available documents.
Bers, Lipman↗
Isolated and cascade airfoils with prescribed velocity distribution
Explore the source record for details and available documents.
Goldstein, Arthur W↗
A rapid approximate method for determining velocity distribution on impeller blades of centrifugal compressors
Explore the source record for details and available documents.
COMPRESSORS - BLADES↗
Detailed computational procedure for design of cascade blades with prescribed velocity distributions in compressible potential flows
Explore the source record for details and available documents.
FLOW, SUBSONIC↗
Mathematical improvement of method for computing Poisson integrals involved in determination of velocity distribution on airfoils
Explore the source record for details and available documents.
RESEARCH TECHNICQUE, MATHEMATICS↗
Design of two-dimensional channels with prescribed velocity distribution along the channel walls I : relaxation solutions
Explore the source record for details and available documents.
Stanitz, John D↗
Design of two-dimensional channels with prescribed velocity distributions along the channel walls II : solution by Green's function
Explore the source record for details and available documents.
Stanitz, John D↗
Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack
Explore the source record for details and available documents.
Stanitz, John D↗
Effect of Type of Porous Surface and Suction Velocity Distribution on the Characteristics of a 10.5-percent-thick Airfoil with Area Suction
Explore the source record for details and available documents.
Dannenberg, Robert E↗
Flight Measurements of the Velocity Distribution and Persistence of the Trailing Vortices of an Airplane
Explore the source record for details and available documents.
Kraft, Christopher C , Jr↗
Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping
Explore the source record for details and available documents.
Moses, H E↗
Velocity distributions on two-dimensional wing-duct inlets by conformal mapping
Explore the source record for details and available documents.
Perl, W↗
Average outside surface heat-transfer coefficients and velocity distributions for heated and cooled impulse turbine blades in static cascades
Explore the source record for details and available documents.
Hubbartt, James E↗
Effect of certain combinations of wall contouring and design exit velocity distribution on prediction of turbine-nozzle mass flow
Explore the source record for details and available documents.
Whitney, Warren J↗
Velocity Distributions Measured in the Slipstream of Eight-blade and Six-blade Dual-rotating Propellers at Zero Advance
Explore the source record for details and available documents.
Salters, Leland B , Jr↗
Effect of inlet-air velocity distribution on the metering pressure of an injection-type aircraft carburetor
Explore the source record for details and available documents.
DUCTS-CORNERS↗
Universal logarithmic law of velocity distribution as applied to the investigation of boundary layer and drag of streamline bodies at large Reynolds number
In the present paper we shall consider a figure of revolution, so that the formulas applicable to the more simple cases as, for example, a wing or flat plate will follow from our equations as corollaries. For checking the results of our theory, we made use of the data derived from the tests of Freeman on a 1/40-scale model of the airship "Akron" conducted in the large NACA wind tunnel. In the first part we shall derive the fundamental equation for a body of revolution according to the Karman theory in its original form, and in the second part we shall give all the comparisons of the results of tests with the modified theory.
Gurjienko, G↗