Aerodynamic Loading Characteristics in Sideslip of a 45 Sweptback Wing with and Without a Fence at High Subsonic Speeds

Aerodynamic Loading Characteristics in Sideslip of a 45   Sweptback Wing with and Without a Fence at High Subsonic Speeds
Author: Richard E. Kuhn,Andrew L. Byrnes
Publsiher: Unknown
Total Pages: 50
Release: 1955
Genre: Aerodynamic load
ISBN: UOM:39015086490185

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Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publsiher: Unknown
Total Pages: 580
Release: 1956
Genre: Aeronautics
ISBN: UCBK:C029901318

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A Selected Listing of NASA Scientific and Technical Reports for

A Selected Listing of NASA Scientific and Technical Reports for
Author: Anonim
Publsiher: Unknown
Total Pages: 818
Release: 1954
Genre: Aeronautics
ISBN: UVA:X004173286

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publsiher: Unknown
Total Pages: 508
Release: 1954
Genre: Aeronautics
ISBN: IND:30000098603164

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WADC Technical Report

WADC Technical Report
Author: United States. Wright Air Development Division
Publsiher: Unknown
Total Pages: 1268
Release: 1957
Genre: Aeronautics
ISBN: UOM:39015022486669

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Subject Index to Unclassified ASTIA Documents

Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)
Publsiher: Unknown
Total Pages: 308
Release: 1960
Genre: Science
ISBN: STANFORD:36105016669785

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Wind tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45 Sweptback Wing at High Subsonic Speeds

Wind tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45   Sweptback Wing at High Subsonic Speeds
Author: James W. Wiggins,Richard E. Kuhn
Publsiher: Unknown
Total Pages: 32
Release: 1954
Genre: Aerodynamic load
ISBN: UOM:39015086490359

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Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Swept wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail

Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45   Swept wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail
Author: M. Leroy Spearman
Publsiher: Unknown
Total Pages: 34
Release: 1957
Genre: Airplanes
ISBN: UOM:39015086466235

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An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.