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
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
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
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
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
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
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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