columbus · Solution Of The Potential Equation For The Unsteady Flow About A Triangular wing with Subsonic Leading Edges In A Supersonic Main Stream

Solution Of The Potential Equation For The Unsteady Flow About A Triangular wing with Subsonic Leading Edges In A Supersonic Main Stream

Title: Solution Of The Potential Equation For The Unsteady Flow About A Triangular wing with Subsonic Leading Edges In A Supersonic Main Stream
Date: 1957
Index Abstract: Limited
Photo Quality: Not Needed
Report Number: WADC TR 57-258
Creator: Luke, Yudell L.; Coombs, Geraldine V.; Wagner, Frank
Corporate Author: Midwest Research Institute
Laboratory: Aeronautical Research Laboratory
Extent: 38
PB Number: PB131851
Identifier: AD0118241
Access Rights: OTS
Distribution Classification: 2
Contract: AF 33(616)-3058
DoD Project: 7-(8-1370)
DoD Task: 70411
DTIC Record Exists: No
Distribution Conflict: Yes
Cover Price: 1.25
Report Availability: Not available via Contrails
Date Issued: 1957-12
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report