columbus · STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings

STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings

Title: STOL Tactical Aircraft Investigation Volume II, Part II A Lifting Line Analysis Method for Jet-Flapped Wings
Date: 1973
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AFFDL TR 73-19 Volume 2 Part 2
Corporate Author: The Boeing Company
Extent: 118
Identifier: AD0766877
Access Rights: Approved for public release; distribution unlimited
Distribution Classification: 1
Contract: F33615-71-C-1757
DoD Project: 643A
DoD Task: None Given
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1973-06
Abstract: The abstract for this report is either unavailable or has yet to be entered
Laboratory: Air Force Flight Dynamics Laboratory
Provenance: AFRL/VACA
Special Scanning Requirements: Some pages blank; printing error
Type: report
Format: 1 online resource
Creator: Davenport, Franklyn J.