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General Electric Fan-In-Fuselage Model in the 40x80 Foot Wind Tunnel at NASA Ames.

General Electric Fan-In-Fuselage Lifting Model in the 40x80 Foot Wind Tunnel at NASA Ames.

Tilt-Wing/Propeller Model With Blowing Flaps Tested in the 40x80 foot Wind Tunnel at NASA Ames.

Generalized Subsonic Jet Transport in 40x80 Foot Wind Tunnel at NASA Ames.

Lift Fan Model In Ames 40 X 80 Wind Tunnel.

The NASA Ames 40x80 Foot Wind Tunnel

Investigation of Ducted Fan in Ames 40x80 Foot Wind Tunnel.

Swept Augmentor Wing Model Installed in the Ames 40X80 Foot Wind Tunnel.

Construction of the Fan Drive Enclosure of the 40x80 Foot Wind Tunnel at Ames.

General Electric Fan-In-Fuselage model in the 40x80 Foot Wind Tunnel at NASA Ames.

description

Summary

G.E. Fan-in-fuselage model (lifting). 3/4 front view of fan at low G.P. position. Lift fan on variable height strut for ground effects studies. T-Tail

Don Richey

label_outline

Tags

fan in fuselage ge ames arc aeronautics 40x80ft wind tunnel ames aeronautics ames research center general electric model foot wind tunnel foot wind tunnel nasa ames high resolution general electric fan in fuselage model fan fan in fuselage model ground effects studies t tail don richey front view height strut nasa
date_range

Date

05/05/1961
place

Location

Ames Research Center
create

Source

NASA
link

Link

https://images.nasa.gov/
copyright

Copyright info

Public Domain Dedication (CC0)

label_outline Explore Ames Aeronautics, Nasa Ames, 40 X 80 Ft

Sonic Boom Model in the Abe Silverstein Supersonic Wind Tunnel (10x10) GRC-2005-C-00946

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

JET THRUSTER MOUNTED ON FREE JET RIG IN THE 10X10 FOOT WIND TUNNEL AREA

Front view of J. C. Buxton's home in Springfield.

Yuri's Night at Ames a celebration of the first human in space ARC-2007-ACD07-0064-058

Facility operators Earl Sine and Joe Manson and CPT Ray Pope (left to right) operate the master control console for 50-megawatt wind tunnel testing. The technicians work in the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Flight Control Division, Air Force Systems Command

PRATT AND WHITNEY P&W COANNULAR NOZZLE TEST IN THE 8X6 FOOT WIND TUNNEL

QCSEE QUIET CLEAN STOL EXPERIMENTAL ENGINE INLET MODEL IN THE 9X15 FOOT LOW SPEED WIND TUNNEL LSWT

Right front view of an A-6 Intruder aircraft from Medium Attack Squadron 165 (VA-165) coming in for an arrested landing aboard the aircraft carrier USS CONSTELLATION (CV-64). Two F-14 Tomcat aircraft are parked on the left

MODEL IN THE 9X15 FOOT WIND TUNNEL

Pair of Dagger-Axes (<i>Ge</i>)

YF-93A (AF48-318 NACA-151) Flight evaluation and comparison of a NACA submerged inlet and a scoop inlet. The YF-93A's were the first aircraft to use flush NACA engine inlets. Note: Used in Flight Research at Ames; 57 Years of Development and Validation of Aeronautical Technology NASA SP-1998-3300 Fig.25 ARC-1969-A-16545

Topics

fan in fuselage ge ames arc aeronautics 40x80ft wind tunnel ames aeronautics ames research center general electric model foot wind tunnel foot wind tunnel nasa ames high resolution general electric fan in fuselage model fan fan in fuselage model ground effects studies t tail don richey front view height strut nasa