Subject Index to Unclassified ASTIA Documents

Author	: Defense Documentation Center (U.S.)
Publisher	:
Total Pages	: 308
Release	: 1960
ISBN-10	: STANFORD:36105016669785
ISBN-13	:
Rating	: 4/5 (85 Downloads)

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Book Synopsis Subject Index to Unclassified ASTIA Documents by : Defense Documentation Center (U.S.)

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Subject Index to Unclassified ASTIA Documents Related Books

Language: en
Pages: 308

Subject Index to Unclassified ASTIA Documents

Authors: Defense Documentation Center (U.S.)

Categories: Science

Type: BOOK - Published: 1960 - Publisher:

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Language: en
Pages: 104

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections

Authors: Jack F. Runckel

Categories: Aerodynamic load

Type: BOOK - Published: 1956 - Publisher:

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An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil s

Language: en
Pages: 1

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and Naca 65a004 Airfoil Sections

Authors: JACK F. RUNCKEL

Categories:

Type: BOOK - Published: 1961 - Publisher:

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An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil s

Language: en
Pages: 88

Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body

Authors: Donald D. Arabian

Categories: Aerodynamics, Transonic

Type: BOOK - Published: 1960 - Publisher:

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The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 d

Language: en
Pages: 36

Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.3, and NACA 65A006 Airfoil Section

Authors: Boyd C. Myers

Categories: Airplane

Type: BOOK - Published: 1949 - Publisher:

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This paper presents the results of the investigation of a wing-alone and wing-fuselage configuration employing a wing with the quarter-chord line swept back 45