Add to ORKGThe starting characteristics for three different model geometries were tested in the Glenn Research Center 225 Square Centimeter Supersonic Wind Tunnel. The test models were tested at Mach 2, 2.5 and 3 in a square test section and at Mach 2.5 again in an asymmetric test section. The results gathered in this study will help size the test models and inform other design features for the eventual implementation of a magnetic suspension system
The effects of inlet turbulence intensity on the aerodynamic performance of a variable speed power t...
The analysis and interpretation of wind tunnel pressure data from the Space Shuttle wind tunnel test...
Flow field measurements of three subsonic rectangular cold air jets are presented. The three cases h...
A feasibility study is in progress at NASA Glenn Research Center to implement a magnetic suspension ...
NASA maintains twelve major wind tunnels at three field centers capable of providing flows at 0.1 M ...
Tests were conducted in the NASA/ARC 6- by 6-foot transonic wind tunnel from September 12 to Septemb...
This presentation accompanies the paper titled Plans and Preliminary Results of Fundamental Studies ...
The measured aerodynamic performance of a compact, high work factor, single-stage centrifugal compre...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hyp...
This presentation describes the process, procedures, and results of the conical probe calibration of...
Recent decades have seen a rapid popularization of Urban Air Mobility (UAM) concepts. The new genera...
NASA Langley has a small, subsonic wind tunnel in use with the 13-inch Magnetic Suspension and Balan...
In support of wear testing for the Hall Effect Rocket with Magnetic Shielding (HERMeS) program, the ...
The primary objective of the test was to obtain stability and control data for the basic configurati...
The effects of inlet turbulence intensity on the aerodynamic performance of a variable speed power t...
The analysis and interpretation of wind tunnel pressure data from the Space Shuttle wind tunnel test...
Flow field measurements of three subsonic rectangular cold air jets are presented. The three cases h...
A feasibility study is in progress at NASA Glenn Research Center to implement a magnetic suspension ...
NASA maintains twelve major wind tunnels at three field centers capable of providing flows at 0.1 M ...
Tests were conducted in the NASA/ARC 6- by 6-foot transonic wind tunnel from September 12 to Septemb...
This presentation accompanies the paper titled Plans and Preliminary Results of Fundamental Studies ...
The measured aerodynamic performance of a compact, high work factor, single-stage centrifugal compre...
Performance data are presented for this tunnel, which has a Mach number range from 2.0 to 3.5. The t...
Experimental aerodynamic investigations were conducted in the NASA Ames Research Center 3.5-Foot Hyp...
This presentation describes the process, procedures, and results of the conical probe calibration of...
Recent decades have seen a rapid popularization of Urban Air Mobility (UAM) concepts. The new genera...
NASA Langley has a small, subsonic wind tunnel in use with the 13-inch Magnetic Suspension and Balan...
In support of wear testing for the Hall Effect Rocket with Magnetic Shielding (HERMeS) program, the ...
The primary objective of the test was to obtain stability and control data for the basic configurati...
The effects of inlet turbulence intensity on the aerodynamic performance of a variable speed power t...
The analysis and interpretation of wind tunnel pressure data from the Space Shuttle wind tunnel test...
Flow field measurements of three subsonic rectangular cold air jets are presented. The three cases h...