Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling

von Beckwith, Ivan E.
Veröffentlicht 1959

Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient

von Beckwith, Ivan E.
Veröffentlicht 1953

Similarity solutions for small cross flows in laminar compressible boundary layers

von Beckwith, Ivan E.
Veröffentlicht 1961

Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling

von Beckwith, Ivan E.
Veröffentlicht 1958

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

von Reshotko, Eli
Veröffentlicht 1958

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

von Reshotko, Eli
Veröffentlicht 1957

Detailed description and results of a method for computing mean and fluctuating quantities in turbulent boundary layers

von Beckwith, Ivan E.
Veröffentlicht 1968

Local heat transfer and recovery temperatures on a yawed cylinder at a Mach number of 4.15 and high Reynolds numbers

von Beckwith, Ivan E.
Veröffentlicht 1961

Calculation by a finite-difference method of supersonic turbulent boundary layers with tangential slot injection

von Beckwith, Ivan E.
Veröffentlicht 1971

An accurate and rapid method for the design of supersonic nozzles

von Beckwith, Ivan E.
Veröffentlicht 1955

Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15

von Beckwith, Ivan E.
Veröffentlicht 1957

The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section

von Beckwith, Ivan E.
Veröffentlicht 1952

The Compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing

von Hunt, James L.
Veröffentlicht 1971

Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel

von MacLellan, Charles H.
Veröffentlicht 1950

Fluctuating properties of turbulent boundary layers for Mach numbers up to 9

von Harvey, William D.
Veröffentlicht 1969

Comparisons of turbulent-boundary-layer measurements at mach number 19.5 with theory and an assessment of probe errors

von Beckwith, Ivan E.
Veröffentlicht 1971