Effect of Horizontal-Tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
This citation is provided as a resource for researchers, but Contrails cannot provide a full-text download
U.S. government employees, Military/Department of Defense employees, and U.S. government contractors and sub-contractors may be eligible to register with the Defense Technical Information Center (DTIC), where this report and others like it may be available
Report Number: NACA TN 2907
Author(s): Riley, Donald R.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Pages: 43
DoD Task:
PB Number: PB108790
Identifier: AD0002801
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Author(s): Riley, Donald R.
Corporate Author(s): Langley Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Pages: 43
DoD Task:
PB Number: PB108790
Identifier: AD0002801
Abstract:
The abstract for this report is either unavailable or has yet to be entered