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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Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8

Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8
Title Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 PDF eBook
Author John L. Allen
Publisher
Pages 24
Release 1960
Genre Airplanes
ISBN

Download Performance Summary and Analysis of a Mach 3.0 Design Axisymmetric All-external-compression Double-cone Inlet Mach Number Range 3.0 to 0.8 Book in PDF, Epub and Kindle

The Effects of Boundary-layer Removal Through Throat Slots on the Internal Performance of a Side Inlet at Mach Numbers of 2.0 and 2.3

The Effects of Boundary-layer Removal Through Throat Slots on the Internal Performance of a Side Inlet at Mach Numbers of 2.0 and 2.3
Title The Effects of Boundary-layer Removal Through Throat Slots on the Internal Performance of a Side Inlet at Mach Numbers of 2.0 and 2.3 PDF eBook
Author John J. Gawienowski
Publisher
Pages 32
Release 1961
Genre Boundary layer control
ISBN

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Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5

Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5
Title Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5 PDF eBook
Author
Publisher
Pages 26
Release 1960
Genre
ISBN

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Performance of a Translating-double-cone Axisymmetric Inlet with Cowl Bypass at Mach Number from 2.0 to 3.5

Performance of a Translating-double-cone Axisymmetric Inlet with Cowl Bypass at Mach Number from 2.0 to 3.5
Title Performance of a Translating-double-cone Axisymmetric Inlet with Cowl Bypass at Mach Number from 2.0 to 3.5 PDF eBook
Author James F. Connors
Publisher
Pages 30
Release 1957
Genre Airplanes
ISBN

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Index to NASA Technical Publications

Index to NASA Technical Publications
Title Index to NASA Technical Publications PDF eBook
Author United States. National Aeronautics and Space Administration
Publisher
Pages
Release 1960-07
Genre
ISBN

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Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1.9 to 6.8

Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1.9 to 6.8
Title Investigation of Three Mach 7 External Compression Axisymmetric Inlets from Mach 1.9 to 6.8 PDF eBook
Author
Publisher
Pages 32
Release 1960
Genre
ISBN

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