columbus · The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges

The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges

Title: The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Date: 1954
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: WADC TR 54-196
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Extent: 41
NTRL Accession Number: AD037709
Identifier: AD0037709
Access Rights: Notice(s)
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFAL LTR
Report Availability: Full text available
Date Issued: 1954-05
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: Epstein, Melvin