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Public Domain Images - Lightning bug firebee

BUFFING FINISH ON THIOKOL ROCKET MISSILE

Senior Airman Eric James Shade Walton, 100th Maintenance

HUBBLE MODEL - U.S. National Archives Public Domain photograph

A Mark 104 acoustic minesweeping device on the flight line prior to a minesweeping demonstration by Helicopter Mine Countermeasures Squadron 12 (HM-12)

US Navy in WWII - 80-G-701579 (18927223734)

F16 AIRPLANE MODEL IN THE 10X10 FOOT WIND TUNNEL

A-15209. High Lift and Stall Control in Ames 40x80 Foot Wind Tunnel.

Deep Stall Model in Ames 40x80 foot Wind Tunnel.

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McDonnell Model XV-1 Convertiplane in the Ames 40x80 Foot Wind Tunnel.

Deep Stall Model in Ames 40x80 foot Wind Tunnel.

Deep Stall Model in Ames 40x80 foot Wind Tunnel.

de Havilland Augmenter Wing Model in Ames 40x80 foot Wind Tunnel.

Lockheed Rigid Rotor Model in Ames 40x80 Foot Wind Tunnel.

Lockheed F-104 in Ames 40x80 Foot Wind Tunnel.

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

F-111B in Ames 40x80 Foot Wind Tunnel.

Testing Tilt Wing Propeller Model in Ames 40x80 Foot Wind Tunnel.

McDonnell F4H Model in Ames 40X80 foot Wind Tunnel.

description

Summary

Application of blowing type boundry-layer control to the leading and trailing edge flaps of a 52 deg swept wing. 3/4 view of Aspect Ratio 2.8, taper ratio .17, 45 deg swept back wing model -3/4 front view

Don Richey

label_outline

Tags

mcdonnell ames aeronautics arc 40 x 80 ft wind tunnel ames aeronautics naca ames research center mcdonnell f model h model foot wind tunnel foot wind tunnel 1950 s airplanes high resolution deg front view don richey mcdonnell f 4 h model type boundry layer control aspect ratio edge flaps view ratio 1950 s aviation nasa
date_range

Date

19/10/1956
place

Location

Ames Research Center
create

Source

NASA
link

Link

https://images.nasa.gov/
copyright

Copyright info

Public Domain Dedication (CC0)

label_outline Explore Aspect Ratio, Deg, Ratio

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

Variable-Density Tunnel, NASA history collection

GPN-2000-000367, NASA history collection

AC-27149-A. General Aerodynamic Characteristics of a Research Model with High Disk Loading Direct Lifting Fan Mounted in Fuselage.

Transformer manufacture. Oval wrapped copper coils which go into power transformers; demand for these transformers has increased in direct ratio to America's increased production of war materials. Transformers are used in almost every phase of the armament program. Westinghouse, Sharon, Pennsylvania

VSTOL VERTICAL SHORT TAKE OFF LANDING MODEL IN THE 10X10 FOOT WIND TUNNEL

NACA Researcher Sets up a Test of a New Seat Design

Fokker-Republic Alliance concept

SPACE SHUTTLE MODEL IN THE 10X10 FOOT WIND TUNNEL

OTW OVER THE WING MODEL IN THE 8X6 FOOT WIND TUNNEL

FLOW RATIO COMPUTER, NASA Technology Images

Closed Loop Breathing System NASA history collection

Topics

mcdonnell ames aeronautics arc 40 x 80 ft wind tunnel ames aeronautics naca ames research center mcdonnell f model h model foot wind tunnel foot wind tunnel 1950 s airplanes high resolution deg front view don richey mcdonnell f 4 h model type boundry layer control aspect ratio edge flaps view ratio 1950 s aviation nasa