The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Report Number: WADC TR 54-196
Author(s): Epstein, Melvin
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Pages: 41
Contract: Laboratory Research - No Contract
DoD Project: None Given
Identifier: AD0037709
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Epstein, Melvin
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Pages: 41
Contract: Laboratory Research - No Contract
DoD Project: None Given
Identifier: AD0037709
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control