Similar
Army Combat Engineers with the 1st Engineer Battalion,
EMPLOY THE HANDICAP WEEK FEATURING MR SWALLOW
TRANSITION FROM IGNITION TO FLAME GROWTH UNDER EXTERNAL RADIATION IN THREE DIMENSIONS TIGER-3D TEST RESULTS FROM THE JAPAN MICROGRAVITY CENTER JAMIC
FORWARD THRUST CONFIGURATION OF THRUST REVERSER AIRPLANE MODEL
Nevada Guard Diversity Day, a ‘cultural buffet', attracts record crowd
CEV (Crew Escape Vehicle) Alternative Launch Abort System (ALAS) configuration test in the Ames 11ft wind tunnel. Test-11-0172 ARC-2007-ACD07-0171-004
NASA MCAIR AXISYMETRIC INLET MODEL - Glenn Research Center History
TRANSITION FROM IGNITION TO FLAME GROWTH UNDER EXTERNAL RADIATION IN THREE DIMENSIONS TIGER-3D TEST RESULTS FROM THE JAPAN MICROGRAVITY CENTER JAMIC
TRANSITION FROM IGNITION TO FLAME GROWTH UNDER EXTERNAL RADIATION IN THREE DIMENSIONS TIGER-3D TEST RESULTS FROM THE JAPAN MICROGRAVITY CENTER JAMIC
Related
DRAG DATA FOR 16 INCH RAM JET ENGINE WITH A 2 OBLIQUE SHOCK TYPE INLET
TWO STAGE INLET BEFORE SEPARATION TEST ON 16 INCH FREE FLIGHT RAM JET
FOIL IN AIR BEARING FOR ENGINE 2 16
FOIL IN AIR BEARING FOR ENGINE 2 16
FOIL IN AIR BEARING FOR ENGINE 2 16
16 INCH RAM JET COMPONENT PARTS SUBASSEMBLY AND FINAL ASSEMBLY
FOIL IN AIR BEARING FOR ENGINE 2 16
RUE FONTAINE/ 16 BIS/ DECADENT'S/ CONCERT/ LE LEVER DE MADAME
16 INCH RAM JET IN TEST SECTION OF 8X6 FOOT SUPERSONIC WIND TUNNEL
DRAG DATA FOR 16 INCH RAM JET ENGINE WITH A 2 OBLIQUE SHOCK TYPE INLET
Summary
DRAG DATA FOR 16 INCH RAM JET ENGINE WITH A 2 OBLIQUE SHOCK TYPE INLET
NASA Identifier: C-1954-36412
Tags
nasa
drag data for 16 inch ram jet engine with a 2 oblique shock type inlet
dvids
high resolution
glenn research center
aviation research organization
jet engine
Date
1954
Location
Source
Defense Visual Information Distribution Service
Link
Copyright info
Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright