Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95 PDF Download

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Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95

Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95 PDF Author: James F. Connors
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95

Performance of an Axisymmetric External-compression and a Two-dimensional External-internal-compression Inlet at Mach 4.95 PDF Author: James F. Connors
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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Book Description

Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0

Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0 PDF Author:
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ISBN:
Category :
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Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79

Performance of a Mach Number 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range 1.97 to 0.79 PDF Author: Owen H. Davis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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Performance of a Mach 3.0 External-internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5

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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

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Category : Airplanes
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Investigation of the Performance and Control of a Mach 3.0, Two-dimensional, External-internal-compression Inlet

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Performance of External-compression Bump Inlet at Mach Numbers of 1.5 to 2.0

Performance of External-compression Bump Inlet at Mach Numbers of 1.5 to 2.0 PDF Author: Paul C. Simon
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Effect of External Boundary Layer on Performance of Axisymmetric Inlet at Mach Numbers of 3.0 and 2.5

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A Two-dimensional External-internal-compression Inlet with Throat Bypass at Mach Number 3.05

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