Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle

Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
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Total Pages : 22
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ISBN-10 : UIUC:30112106872465
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Book Synopsis Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle by : Byron M. Jaquet

Download or read book Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle written by Byron M. Jaquet and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle Related Books

Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
Language: en
Pages: 22
Authors: Byron M. Jaquet
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1961 - Publisher:

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Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle
Language: en
Pages: 1
Authors: Byron M. Jaquet
Categories:
Type: BOOK - Published: 1961 - Publisher:

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A wind-tunnel investigation was made at a Mach number of 3.10 (Reynolds number per foot of 16.3 x 10 to the 6th power to 16.9 x 10 to the 6th power) to determin
Aerodynamic Loading Characteristics of a 1/10-scale Model of the Three-stage Scout Vehicle at Mach Numbers 1.57 to 4.65
Language: en
Pages: 52
Authors: Lloyd S. Jernell
Categories: Aerodynamic load
Type: BOOK - Published: 1963 - Publisher:

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Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-scale Model of the Scout Vehicle at a Mach Number of 2.01
Language: en
Pages: 42
Authors: Ross B. Robinson
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

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Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model
Language: en
Pages: 68
Authors: Thomas C. Kelly
Categories: Launch vehicles (Astronautics)
Type: BOOK - Published: 1961 - Publisher:

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Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upp