Unsteady Aerodynamics for Advanced Configurations: Part III - Elliptic-Conical Wing in Linearized Unsteady Transonic Flow

This report has yet to be scanned by Contrails staff

Report Number: FDL TDR 64-152 Part 3
Author(s): Albano, E., Andrew, L. V.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05
Pages: 43
Contract: AF 33(657)-10399
DoD Project: 1370
DoD Task: 137003
Identifier: AD0618083

Abstract:
The abstract for this report is either unavailable or has yet to be entered

Provenance: AFRL/VACA

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement



Export