columbus · Theoretical Calculation of the Pressure Distribution, Span Loading, and Rolling Moment Due to Sideslip at Supersonic Speeds for Thin Sweptback Tapered Wings with Supersonic Trailing Edges and Wing Tips Parallel to the Axis of Wing Symmetry

Theoretical Calculation of the Pressure Distribution, Span Loading, and Rolling Moment Due to Sideslip at Supersonic Speeds for Thin Sweptback Tapered Wings with Supersonic Trailing Edges and Wing Tips Parallel to the Axis of Wing Symmetry

Title: Theoretical Calculation of the Pressure Distribution, Span Loading, and Rolling Moment Due to Sideslip at Supersonic Speeds for Thin Sweptback Tapered Wings with Supersonic Trailing Edges and Wing Tips Parallel to the Axis of Wing Symmetry
Date: 1953
Index Abstract: Limited
Photo Quality: Undetermined
Report Number: NACA TN 2898
Creator: Margolis, Kenneth; Sherman, Windsor L.; Hannah, Margery E.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Extent: 75
PB Number: PB108784
Identifier: AD0002803
Access Rights: Unknown
Distribution Classification: 2
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1953-02
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: PB/AD Index
Type: report