columbus · Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack

Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack

Item

Title: Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack
Date: 1965
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: FDL TDR 64-152 Part 5
Creator: Li, T. C.
Corporate Author: North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 52
Identifier: AD0619397
Access Rights: Notice(s)
Distribution Classification: 1
Contract: AF 33(657)-10399
DoD Project: 1370
DoD Task: 137003
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: In the portion of the study covered in this report, linearized theory is developed for potential flow around a slender body at not too large angles of attack. The solution is obtained by 'definitizing' the flow equation and rigorously satisfying the boundary conditions. This approach is completely different from conventional methods in that it constitutes a process of obtaining an analytic solution to the problem of potential flow by a 'march from the body' toward infinity. The extension of this new theory to the nonlinear case is immediate. Having shown it is possible to not restrict the Mach number, it is expected that the new theory should be applicable to the cases of subsonic, transonic and supersonic speeds as well.
Report Availability: Full text available
Date Issued: 1965-05
Provenance: AFRL/VACA
Type: report
Format: 1 online resource

Media: FDLTDR64-152part05.pdf