Experimental Investigation Of A Method Of Interference Drag Reduction Of A Swept Wing Aircraft By Means Of Fuselage Indentation
Report Number: WADC TR 55-12
Author(s): Degen, M.
Corporate Author(s): Brown Univ Providence RI
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-03
Pages: 110
Contract: AF 33(616)-2319
DoD Project: 1366
DoD Task: 70113
Identifier: AD0092966
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Degen, M.
Corporate Author(s): Brown Univ Providence RI
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1956-03
Pages: 110
Contract: AF 33(616)-2319
DoD Project: 1366
DoD Task: 70113
Identifier: AD0092966
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control