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Calibration report on the University of Michigan 8- by 13-inch supersonic wind tunnel

Liepman, Hans Peter
Amick, James L.
Reynolds, Theodore H.

Publication date

January 1954

Abstract

http://deepblue.lib.umich.edu/bitstream/2027.42/6303/5/bac9931.0001.001.pdfhttp://deepblue.lib.umich.edu/bitstream/2027.42/6303/4/bac9931.0001.001.tx

Extracted data

Related items

Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section /

Botner, W. T.
Maydew, R. C.
Spahr, H. R.
U.S. Atomic Energy Commission.
Sandia Corporation.

"The speed range of the Sandia 12 x 12-inch transonic wind tunnel was recently increased from Mach 1...

A study of a small supersonic wind tunnel

Chang, Pu-Kwang

January 1967

Due to the character of the original source materials and the nature of batch digitization, quality ...

Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /

Jackson, F. M., III, author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

Tests were conducted in the AEDC Propulsion Wind Tunnel (16T) to determine the tunnel test section M...

Calibration report on the University of Michigan supersonic wind tunnel : part 1, Wind tunnel facilities and testing techniques : part 2, Aerodynamic calibration at nominal Mach number of 1.90

Culbertson, Philip E.

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/4446/5/bab4663.0001.001.pdfhttp://deepblue.lib.umich...

Calibration report on the University of Michigan supersonic wind tunnel : part I, Wind tunnel facilities and testing techniques : part II, Aerodynamic calibration of nominal Mach number 1.90

Culbertson, Philip E.

January 1949

http://deepblue.lib.umich.edu/bitstream/2027.42/4447/5/bab4664.0001.001.pdfhttp://deepblue.lib.umich...

Calibration report on the University of Michigan supersonic wind tunnel : part III, aerodynamic calibration at nomial Mach number on 2.84 : part IV, aerodynamic calibration at nominal Mach number of 1.44

Culbertson, Philip E.

January 1952

http://deepblue.lib.umich.edu/bitstream/2027.42/4448/5/bab7782.0001.001.pdfhttp://deepblue.lib.umich...

University of Michigan 8 x 13 inch intermittent-flow supersonic wind tunnel

Garby, Louis Charles
Nelson, Walter C.

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/4998/5/bac2779.0001.001.pdfhttp://deepblue.lib.umich...

Supersonic wind tunnel research facilities

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/7835/5/bad2449.0001.001.pdfhttp://deepblue.lib.umich...

Part 1. Construction and calibration of the McGill supersonic wind tunnel.

Kwok, Chi. K.

January 1962

The design and construction of the McGill intermittent, suckdown supersonic wind tunnel and its inst...

Calibration of transonic and supersonic wind tunnels /

Reed, T. D.
Cooksey, J. M., joint author.
Pope, T. C., joint author.
Vought Corporation.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1977

Issued Nov. 1977.Prepared for Ames Research Center under Contact NAS 2-8606.Includes bibliographical...

The calibration and description of a wind-tunnel for studying stratified flows

Debler, Walter R.
Montgomery, Richard Douglas.

January 1971

http://deepblue.lib.umich.edu/bitstream/2027.42/4519/5/bab8658.0001.001.pdfhttp://deepblue.lib.umich...

Automatic reduction of wind tunnel data : final report.

Leite, Richard Joseph
Cotecchia, Ugo A.
Haneman, Vincent Siering.
Howe, Robert Milton

January 1951

http://deepblue.lib.umich.edu/bitstream/2027.42/6261/5/bad0389.0005.001.pdfhttp://deepblue.lib.umich...

Development Of The USM Wind Tunnel Validation Model For Calibration

Sim, Chiow Moon

June 2018

Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...

Intermittent supersonic wind tunnel

Schneyer, Raymond I.

January 1948

http://deepblue.lib.umich.edu/bitstream/2027.42/7450/5/bad5740.0001.001.pdfhttp://deepblue.lib.umich...

Check Calibration of the NASA Glenn 10- by 10-Foot Supersonic Wind Tunnel (2014 Test Entry)

Johnson, Aaron
Arrington, E. Allen
Pastor-Barsi, Christine

May 2016

A check calibration of the 10- by 10-Foot Supersonic Wind Tunnel (SWT) was conducted in May/June 201...

Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section /

Botner, W. T.
Maydew, R. C.
Spahr, H. R.
U.S. Atomic Energy Commission.
Sandia Corporation.

"The speed range of the Sandia 12 x 12-inch transonic wind tunnel was recently increased from Mach 1...

A study of a small supersonic wind tunnel

Chang, Pu-Kwang

January 1967

Due to the character of the original source materials and the nature of batch digitization, quality ...

Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /

Jackson, F. M., III, author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

Tests were conducted in the AEDC Propulsion Wind Tunnel (16T) to determine the tunnel test section M...

Calibration report on the University of Michigan supersonic wind tunnel : part 1, Wind tunnel facilities and testing techniques : part 2, Aerodynamic calibration at nominal Mach number of 1.90

Culbertson, Philip E.

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/4446/5/bab4663.0001.001.pdfhttp://deepblue.lib.umich...

Calibration report on the University of Michigan supersonic wind tunnel : part I, Wind tunnel facilities and testing techniques : part II, Aerodynamic calibration of nominal Mach number 1.90

Culbertson, Philip E.

January 1949

http://deepblue.lib.umich.edu/bitstream/2027.42/4447/5/bab4664.0001.001.pdfhttp://deepblue.lib.umich...

Calibration report on the University of Michigan supersonic wind tunnel : part III, aerodynamic calibration at nomial Mach number on 2.84 : part IV, aerodynamic calibration at nominal Mach number of 1.44

Culbertson, Philip E.

January 1952

http://deepblue.lib.umich.edu/bitstream/2027.42/4448/5/bab7782.0001.001.pdfhttp://deepblue.lib.umich...

University of Michigan 8 x 13 inch intermittent-flow supersonic wind tunnel

Garby, Louis Charles
Nelson, Walter C.

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/4998/5/bac2779.0001.001.pdfhttp://deepblue.lib.umich...

Supersonic wind tunnel research facilities

January 1950

http://deepblue.lib.umich.edu/bitstream/2027.42/7835/5/bad2449.0001.001.pdfhttp://deepblue.lib.umich...

Part 1. Construction and calibration of the McGill supersonic wind tunnel.

Kwok, Chi. K.

January 1962

The design and construction of the McGill intermittent, suckdown supersonic wind tunnel and its inst...

Calibration of transonic and supersonic wind tunnels /

Reed, T. D.
Cooksey, J. M., joint author.
Pope, T. C., joint author.
Vought Corporation.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1977

Issued Nov. 1977.Prepared for Ames Research Center under Contact NAS 2-8606.Includes bibliographical...

The calibration and description of a wind-tunnel for studying stratified flows

Debler, Walter R.
Montgomery, Richard Douglas.

January 1971

http://deepblue.lib.umich.edu/bitstream/2027.42/4519/5/bab8658.0001.001.pdfhttp://deepblue.lib.umich...

Automatic reduction of wind tunnel data : final report.

Leite, Richard Joseph
Cotecchia, Ugo A.
Haneman, Vincent Siering.
Howe, Robert Milton

January 1951

http://deepblue.lib.umich.edu/bitstream/2027.42/6261/5/bad0389.0005.001.pdfhttp://deepblue.lib.umich...

Development Of The USM Wind Tunnel Validation Model For Calibration

Sim, Chiow Moon

June 2018

Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...

Intermittent supersonic wind tunnel

Schneyer, Raymond I.

January 1948

http://deepblue.lib.umich.edu/bitstream/2027.42/7450/5/bad5740.0001.001.pdfhttp://deepblue.lib.umich...

Check Calibration of the NASA Glenn 10- by 10-Foot Supersonic Wind Tunnel (2014 Test Entry)

Johnson, Aaron
Arrington, E. Allen
Pastor-Barsi, Christine

May 2016

A check calibration of the 10- by 10-Foot Supersonic Wind Tunnel (SWT) was conducted in May/June 201...

Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section /

Botner, W. T.
Maydew, R. C.
Spahr, H. R.
U.S. Atomic Energy Commission.
Sandia Corporation.

"The speed range of the Sandia 12 x 12-inch transonic wind tunnel was recently increased from Mach 1...

A study of a small supersonic wind tunnel

Chang, Pu-Kwang

January 1967

Due to the character of the original source materials and the nature of batch digitization, quality ...

Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /

Jackson, F. M., III, author.
United States. Air Force. Systems Command. issuing body.
Arnold Engineering Development Center, sponsor.
ARO, Inc., sponsor.

Tests were conducted in the AEDC Propulsion Wind Tunnel (16T) to determine the tunnel test section M...