columbus · Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part II: Leading-Edge Slat Design Method.

Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part II: Leading-Edge Slat Design Method.

Title: Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part II: Leading-Edge Slat Design Method.
Date: 1972
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AFFDL TR 72-96 Part 2
Creator: McGregor, O. Wayne; McWhirter, Jack W.
Corporate Author: General Dynamics Fort Worth Tex Convair Aerospace Div
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 176
Identifier: AD0749485
Access Rights: Approved for public release; distribution unlimited
Distribution Classification: 1
Contract: F33615-71-C-1597
DoD Project: 1366
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1972-08
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Special Scanning Requirements: Original and pdf missing pages 81-87
Type: report
Format: 1 online resource