columbus · Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities

Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities

Title: Subsonic Oscillatory or Steady Airloads on Wings with Control Surfaces and Other Discontinuities
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: AFOSR 68-0419
Index Price: $0.00
Report Availability: Full text available by request
Creator: Ashley, Holt
Date: 1967
Extent: 45
Corporate Author: Stanford University, Department of Aeronautics and Astronautics
Laboratory: Air Force Office of Scientific Research
Identifier: AD0669373
Corporate Report Number: SUDAAR NO. 336
Contract: AF44620-67-C-0044
Distribution Conflict: No
Access Rights: Reproduction in whole or in part is permitted for any purpose of the United States Government
Distribution Classification: 1
Date Issued: 1967-12
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report
Format: 45 pages ; 28 cm.