Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6 PDF Author: John D. Morrow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

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Large-scale Flight Measurements of Zero-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6

Large-scale Flight Measurements of Zero-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6 PDF Author: John D. Morrow
Publisher:
ISBN:
Category :
Languages : en
Pages : 53

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Large Scale Flight Measurements of Zero-lift Drag and Low-lift Longitudinal Characteristics of a Diamond-wing-body Combination at Mach Numbers from 0.725 to 1.54

Large Scale Flight Measurements of Zero-lift Drag and Low-lift Longitudinal Characteristics of a Diamond-wing-body Combination at Mach Numbers from 0.725 to 1.54 PDF Author: Harvey A. Wallskog
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Free-flight Measurements of the Zero-lift Drag of Several Wings at Mach Numbers from 1.4 to 3.8

Free-flight Measurements of the Zero-lift Drag of Several Wings at Mach Numbers from 1.4 to 3.8 PDF Author: H. Herbert Jackson
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ISBN:
Category : Mach number
Languages : en
Pages : 32

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Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag Longitudinal Characteristics of a Diamond-wing-body Combination at Mach Numbers from 0.725 to 1.54

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag Longitudinal Characteristics of a Diamond-wing-body Combination at Mach Numbers from 0.725 to 1.54 PDF Author: Harvey A. Wallskog
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Collection of Zero-lift Drag Data on Bodies of Revolution from Free-flight Investigations

Collection of Zero-lift Drag Data on Bodies of Revolution from Free-flight Investigations PDF Author: William E. Stoney
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ISBN:
Category : Body of revolution
Languages : en
Pages : 196

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This report presents a compilation of most of the zero-lift drag results obtained from free-flight measurements made by the Langley Pilotless Aircraft Research Division on fin-stabilized bodies of revolution. The data are arranged on standard forms, which also contain the significant geometrical factors. Supplementary data have been provided to facilitate the determination of the body pressure drags from the measurement total drags. Summary plots and discussions have been included to provide a unified and broad picture of the effects of the body geometry on zero-lift drag.

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.8 to 1.6 of a Wing-body Combination Having an Unswept 4.5-percent-thick Wing with Modified Hexagonal Sections

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.8 to 1.6 of a Wing-body Combination Having an Unswept 4.5-percent-thick Wing with Modified Hexagonal Sections PDF Author: Eugene D. Schult
Publisher:
ISBN:
Category :
Languages : en
Pages : 14

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Comparison of Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.9 to 1.7 of Two Wing-body Combinations Having Similar 60 Degrees Triangular Wings with NACA 65A003 Sections

Comparison of Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.9 to 1.7 of Two Wing-body Combinations Having Similar 60 Degrees Triangular Wings with NACA 65A003 Sections PDF Author: Eugene D. Schult
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.86 to 1.5 of a Wing-body Combination Having a 60 Degrees Triangular Wing with NACA 65A003 Sections

Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.86 to 1.5 of a Wing-body Combination Having a 60 Degrees Triangular Wing with NACA 65A003 Sections PDF Author: Robert L. Nelson
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ISBN:
Category :
Languages : en
Pages :

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Comparison of Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.9 to 1.7 of Two Wing-body Combinations Having Similar 60 Degree Triangular Wings with NACA 65A003 Sections

Comparison of Large-scale Flight Measurements of Zero-lift Drag at Mach Numbers from 0.9 to 1.7 of Two Wing-body Combinations Having Similar 60 Degree Triangular Wings with NACA 65A003 Sections PDF Author: Eugene D. Schult
Publisher:
ISBN:
Category :
Languages : en
Pages : 15

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