visibility Similar

(SLAP) Scanning L-band Active Passive Installed on NASA UC-12B A

SIGB (Standard Interface Glove Box) & MRS (Middeck Rack Structure). ARC-1997-AC97-0015-15

APOLLO - TOOLS - MSC. NASA public domain image colelction.

KENNEDY SPACE CENTER, FLA. - On Pad 17-B, Cape Canaveral Air Force Station, workers move the Boeing Delta II Heavy second-stage engine, the Aerojet AJ10-118K, inside the mobile service tower. The engine will be mated with the first stage of the Delta II, which is the launch vehicle for the MESSENGER (Mercury Surface, Space Environment, Geochemistry and Ranging) spacecraft, scheduled to lift off Aug. 2. Bound for Mercury, the spacecraft is expected to reach orbit around the planet in March 2011. MESSENGER was built for NASA by the Johns Hopkins University Applied Physics Laboratory in Laurel, Md. KSC-04pd1451

SITTING EFFECTS IN DROPLET COMBUSTION DCE DROP RIG

NASA HEAT REJECTION RADIATOR & OTHERS - Glenn Research Center History

3 ZERO GRAVITY DROP MODELS - CYLINDRICAL - RECTANGULAR - SPHERICAL

Hydrostar radiometer, NASA history collection

Hydrostar radiometer, NASA history collection

code Related

N-231 High Reynolds Number Channel Facility (4x6 Inch Channel - Atmospheric) ARC-1980-AC80-0512-4

N-258 NAS (Numerical Aerodynamic Simualtion) Facility, aerials of (pre) construction site, Framing ARC-1985-AC85-5018-2

N-258 NAS (Numerical Aerodynamic Simualtion) Facility, aerials of (pre) construction site, Framing ARC-1985-A85-5017-6

N-231 High Reynolds Number Channel Facility (An example of a Versatile Wind Tunnel) Tunnel 1 I is a blowdown Facility that utilizes interchangeable test sections and nozzles. The facility provides experimental support for the fluid mechanics research, including experimental verification of aerodynamic computer codes and boundary-layer and airfoil studies that require high Reynolds number simulation. (Tunnel 1) ARC-1980-AC80-0512-2

N-258 NAS (Numerical Aerodynamic Simulation) Facility, Aerials of construction site, framing ARC-1985-AC85-5029-6

N-258 NAS (Numerical Aerodynamic Simualtion) Facility, aerials of (pre) construction site, Foundation ARC-1985-AC85-5015-7

N-258 NAS (Numerical Aerodynamic Simulation) Facility, Roof Top Aerial of Construction Site, Framing ARC-1985-AC85-5032-1

N-231 High Reynolds Number Channel II Facility In this timeframe the test section was designed specifically to test two-dimensional airfoil models. It is equipped with 'through-the-wall' turntables that remotely position the airfoil, with flexible upper and lower walls that can be adjusted to minimize wall interference. Porous side-wall panels provide boundary-layer removal. ARC-1980-AC80-0512-3

N-258 NAS (Numerical Aerodynamic Simulation) Facility, Aerials of construction site, framing ARC-1985-AC85-5029-1

N-231 High Reynolds Number Channel Facility (Tunnel 2, Airfoil Test Section) ARC-1980-AC80-0512-1

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Summary

N-231 High Reynolds Number Channel Facility (Tunnel 2, Airfoil Test Section)

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high reynolds number channel facility arc bill clark ames research center high reynolds channel tunnel airfoil test section airfoil test section n 231 high reynolds number channel facility nasa
date_range

Date

05/06/1980
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Source

NASA
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Link

https://images.nasa.gov/
copyright

Copyright info

Public Domain Dedication (CC0)

label_outline Explore Airfoil, Bill Clark, Reynolds

TEST ITEM IN THE ICING RESEARCH TUNNEL IRT

Hydrogen circulatory system for Van de Graaff arc source. Photograph taken February 28, 1946. LINAC-64

Upper Mississippi River Nine-Foot Channel Project, Lock & Dam Complex No. 20, Upper Mississippi River, Canton, Lewis County, MO

CAPE CANAVERAL, Fla. – In High Bay 4 of the Vehicle Assembly Building at NASA's Kennedy Space Center in Florida, the Ares I-X upper stage simulator service module/service adapter segment (foreground) is being prepared for its move to a stand. Other segments are placed and stacked on the floor around it. Ares I-X is the test vehicle for the Ares I, which is part of the Constellation Program to return men to the moon and beyond. The Ares I-X is targeted for launch in July 2009. Photo credit: NASA/Kim Shiflett KSC-2009-2462

HIGH PRESSURE 1.6 FAN SIMULATION ASSEMBLY

STS081-361-027 - STS-081 - MS Grunsfeld moves freezer unit through transfer tunnel to Spacehab

ENGINE INLET PROOF TEST AT THE ICING RESEARCH TUNNEL IRT

AST-05-314 - Apollo Soyuz Test Project - Apollo Soyuz Test Project, MA-148 Equipment, Tunnel Door Aiar

2 HIGH TEMPERATURE PRESSURE FURNACES IN THE MATERIALS AND STRESSES M&S BUILDING ROOM 31

PRESSURE SYSTEMS - HIGH PRESSURE AIR SYSTEMS - NITROGEN PURGE - 450 COMBUSTION AIR

Upper Mississippi River 9-Foot Channel Project, Lock & Dam No. 3, Red Wing, Goodhue County, MN

Navy Ship ARC-4 Thor - Public domain photogrpaph

Topics

high reynolds number channel facility arc bill clark ames research center high reynolds channel tunnel airfoil test section airfoil test section n 231 high reynolds number channel facility nasa