Arkivism
Low Speed Investigation of a Supersonic Transport Model in the 40x80 Wind Tunnel at NASA Ames.
Public domain

Low Speed Investigation of a Supersonic Transport Model in the 40x80 Wind Tunnel at NASA Ames.

NASA / ARC · 1961-03-01 · photograph (digital archive)

From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.

About this work

Low Speed investigation of a supersonic transport model in the 40x80 Wind Tunnel. 03/01/1961 R 975 T Zero angel of attack. Supersonic transport with delta wing and delta conard. 3/4 front view.

NASA Image and Video Library’s own description
Subjects
SSTDelta WingAmesARC40x80ftWind TunnelAeronautics
Credit lineLow Speed Investigation of a Supersonic Transport Model in the 40x80 Wind Tunnel at NASA Ames.. NASA/ARC, 1961-03-01. Public domain. ID: A-27615.
Open in Explore View at source

Similar works

Supersonic Transport Configuration in Large scale (40x80 foot) Wind Tunnel Investigation at Ames Research CenterSupersonic Transport Configuration in Large scale (40x80 foot) Wind Tunnel Investigation at Ames Research Center ARC-1962-A-28474ARC-1962-A-28474 Change Vought XF8U-1 Wing.Change Vought XF8U-1 Wing. McDonnell F4H Model in Ames 40X80 foot Wind Tunnel.McDonnell F4H Model in Ames 40X80 foot Wind Tunnel. Low Speed Investigation of a Supersonic Transport Model in the 40x80 Foot Wind Tunnel.Low Speed Investigation of a Supersonic Transport Model in the 40x80 Foot Wind Tunnel. Fixed Wing Supersonic Transport in Ames 40x80 Foot Wind Tunnel.Fixed Wing Supersonic Transport in Ames 40x80 Foot Wind Tunnel.