Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 292

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Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lenghts at Mach Numbers from 0.60 to 0.92

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lenghts at Mach Numbers from 0.60 to 0.92 PDF Author: Richard J. Re
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 26

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Experimental Pressure Distributions on Axisymmetric Cowls at Mach Numbers from 0. 60 To 0. 92

Experimental Pressure Distributions on Axisymmetric Cowls at Mach Numbers from 0. 60 To 0. 92 PDF Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289234362
Category :
Languages : en
Pages : 224

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The NASA Technical Reports Server (NTRS) houses half a million publications that are a valuable means of information to researchers, teachers, students, and the general public. These documents are all aerospace related with much scientific and technical information created or funded by NASA. Some types of documents include conference papers, research reports, meeting papers, journal articles and more. This is one of those documents.

Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3

Investigation of a Mixed Compression Axisymmetric Inlet at Mach Number 5.3 PDF Author: Eldon A. Latham
Publisher:
ISBN:
Category : Axial flow
Languages : en
Pages : 44

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Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312)

Aeronautical Enginnering: A Cumulative Index to a Continuing Bibliography (supplement 312) PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 392

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Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0

Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0 PDF Author: Frederick K. Hube
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 278

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An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel

An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel PDF Author: Travis W. Binion (Jr.)
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 88

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A Wind Tunnel Investigation of Three NACA 1-series Inlets at Mach Numbers Up to 0.92

A Wind Tunnel Investigation of Three NACA 1-series Inlets at Mach Numbers Up to 0.92 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 180

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A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up to 0.92

A Wind Tunnel Investigation of Three NACA 1-Series Inlets at Mach Numbers Up to 0.92 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 188

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