Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities
This report has yet to be scanned by Contrails staff
Report Number: AFOSR 68-0419
Author(s): Ashley, Holt
Corporate Author(s): Stanford University, Department of Aeronautics and Astronautics
Laboratory: Air Force Office of Scientific Research
Corporate Report Number: SUDAAR NO. 336
Date of Publication: 1967-12
Pages: 45
Contract: AF44620-67-C-0044
DoD Task:
Identifier: AD0669373
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Author(s): Ashley, Holt
Corporate Author(s): Stanford University, Department of Aeronautics and Astronautics
Laboratory: Air Force Office of Scientific Research
Corporate Report Number: SUDAAR NO. 336
Date of Publication: 1967-12
Pages: 45
Contract: AF44620-67-C-0044
DoD Task:
Identifier: AD0669373
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero