columbus · Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation

Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation

Title: Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation
Date: 1956
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: WADC TR 55-12
Corporate Author: Brown Univ Providence RI
Laboratory: Aeronautical Research Laboratory
Extent: 110
NTRL Accession Number: AD092966
Identifier: AD0092966
Access Rights: ASTIA
Distribution Classification: 1
Contract: AF 33(616)-2319
DoD Project: 1366
DoD Task: 70113
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFWAL LTR
Report Availability: Full text available
Date Issued: 1956-03
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource
Creator: Degen, M.