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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Conference on Hypersonic Aircraft Technology

Conference on Hypersonic Aircraft Technology
Title Conference on Hypersonic Aircraft Technology PDF eBook
Author
Publisher
Pages 590
Release 1967
Genre Airplanes
ISBN

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Title Scientific and Technical Aerospace Reports PDF eBook
Author
Publisher
Pages 1074
Release 1965
Genre Aeronautics
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 34
Release 1960
Genre Boundary layer control
ISBN

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Title NASA Scientific and Technical Reports PDF eBook
Author United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher
Pages 1440
Release 1966
Genre Aeronautics
ISBN

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Experimental Investigation of a Mach 6 Fixed-geometry Inlet Featuring a Swept External-internal Compression Flow Field

Experimental Investigation of a Mach 6 Fixed-geometry Inlet Featuring a Swept External-internal Compression Flow Field
Title Experimental Investigation of a Mach 6 Fixed-geometry Inlet Featuring a Swept External-internal Compression Flow Field PDF eBook
Author Marvin G. Torrence
Publisher
Pages 66
Release 1975
Genre Aerodynamics, Hypersonic
ISBN

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Investigation of the Compression Field and the Flow Distribution in the Throat of a Two Dimensional, Internal Compression, Mach Number 6.9 Inlet

Investigation of the Compression Field and the Flow Distribution in the Throat of a Two Dimensional, Internal Compression, Mach Number 6.9 Inlet
Title Investigation of the Compression Field and the Flow Distribution in the Throat of a Two Dimensional, Internal Compression, Mach Number 6.9 Inlet PDF eBook
Author
Publisher
Pages 56
Release 1961
Genre
ISBN

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