columbus · Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part I. General Applications.

Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part I. General Applications.

Title: Demonstration of a Supersonic Box Method for Unsteady Aerodynamics of Nonplanar Wings. Part I. General Applications.
Date: 1969
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: AFFDL TR 67-104 Part 1
Creator: Olsen, James J.
Corporate Author: Air Force Flight Dynamics Lab Wright-Patterson AFB OH
Extent: 78
Identifier: AD0850647
Access Rights: Export Control
Distribution Classification: 1
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Abstract: The report presents and interprets the calculations of the unsteady aerodynamic prediction method known as the 'Nonplanar Mach Box' method. It contains examples of data input and output for the associated computer program and explains the program's interpretation of the user's modal data. Also included are summaries of convergence properties, comparison with exact linearized theory, and a brief outline of the calculations for the Advisory Group for Aeronautical Research and Development (AGARD) planforms.
Report Availability: Full text available
Date Issued: 1969-02
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource