Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet

Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet
Title Experimental Investigation of Boundary Layers in an Axisymmetric Mach 2.5, Mixed Compression Inlet PDF eBook
Author Warren R. Hingst
Publisher
Pages 33
Release 1973
Genre
ISBN

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Comparison of Theoretical and Experimental Boundary-layer Development in a Mach 2.5 Mixed-compression Inlet

Comparison of Theoretical and Experimental Boundary-layer Development in a Mach 2.5 Mixed-compression Inlet
Title Comparison of Theoretical and Experimental Boundary-layer Development in a Mach 2.5 Mixed-compression Inlet PDF eBook
Author Warren R. Hingst
Publisher
Pages 36
Release 1974
Genre Aerodynamics, Supersonic
ISBN

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An Experimental Investigation at Mach Numbers from 2.1 to 3.0 of Circular Internal-compression Inlets Having Translatable Centerbodies and Provisions for Boundary-layer Removal

An Experimental Investigation at Mach Numbers from 2.1 to 3.0 of Circular Internal-compression Inlets Having Translatable Centerbodies and Provisions for Boundary-layer Removal
Title An Experimental Investigation at Mach Numbers from 2.1 to 3.0 of Circular Internal-compression Inlets Having Translatable Centerbodies and Provisions for Boundary-layer Removal PDF eBook
Author Earl C. Watson
Publisher
Pages 32
Release 1960
Genre Boundary layer control
ISBN

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Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3

Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3
Title Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 PDF eBook
Author Eldon A. Latham
Publisher
Pages 44
Release 1972
Genre Axial flow
ISBN

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Experimental Study of Transitional Axisymmetric Shock-boundary Layer Interactions at Mach 5

Experimental Study of Transitional Axisymmetric Shock-boundary Layer Interactions at Mach 5
Title Experimental Study of Transitional Axisymmetric Shock-boundary Layer Interactions at Mach 5 PDF eBook
Author K. S. Heffner
Publisher
Pages
Release 1993
Genre
ISBN

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Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3.0 and 2.5

Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3.0 and 2.5
Title Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3.0 and 2.5 PDF eBook
Author N. E. Samanich
Publisher
Pages 20
Release 1959
Genre Aerodynamics, Supersonic
ISBN

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Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed

Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed
Title Experimental Investigation of a Mach 5 Isentropic Spike Inlet at and Below Design Speed PDF eBook
Author Leonard E. Stitt
Publisher
Pages 22
Release 1959
Genre Aerodynamics, Supersonic
ISBN

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