Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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21 reports

Flow Characteristics Of A 40-Inch Wind Tunnel At Mach Numbers 1.5 To 6

Author(s): Coats, Jack D.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report Number: AEDC TDR 62-130
full text available

Further Experiments on Impact-Pressure Probes in a Low-Density, Hypervelocity Flow

Author(s): Bailey, A. B.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report Number: AEDC TDR 62-208
full text available

Compensation Of Dynamic Sting Effects In Hotshot Force Measurements

Author(s): Edenfield, E. E.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report Number: AEDC TDR 62-122
full text available

Addendum to an Investigation of the Equilibrium Pressure Along Unequally Heated Tubes

Author(s): Bailey, A. B.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-10
Report Number: AEDC TDR 62-188
full text available

Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow

Author(s): Potter, J. Leith
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report Number: AEDC TDR 62-155
full text available

Source Flow Effects In Conical Hypervelocity Nozzles

Author(s): Whitfield, Jack D.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-06
Report Number: AEDC TDR 62-116
full text available

Measurements of Pressure and Speed of Flow in a Spark-Heated Hypersonic Wind Tunnel

Author(s): Karamcheti, Krishnamurty
Corporate Author: Stanford University
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report Number: AEDC TDR 62-218
full text available

The Drag of Spheres in Rarefied Hypervelocity Flow

Author(s): Kinslow, Max
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-12
Report Number: AEDC TDR 62-205
full text available

Radio Telemetry of Stagnation Pressure from a wind Tunnel Model Magnetically Supported in Supersonic Flow,

Author(s): Clemens, P. L.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report Number: AEDC TDR 62-141
full text available

A Device for Measuring Heat Transfer Rates in Arc-Discharge Hypervelocity Wind Tunnels

Author(s): Ledford, R. L.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report Number: AEDC TDR 62-64
full text available

Microwave Measurement of Projectile Kinematics Within Launcher Barrels

Author(s): Hendrix, R. E.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report Number: AEDC TDR 62-213
full text available

Fatigue Tests and Crack Detection on Some Types of Axial-Flow Compressor Rotor Blades

Author(s): Thomas, R. E.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-10
Report Number: AEDC TDR 62-168
full text available

An Examination Of Epoxy Systems Useful In Packaging High G Radio Telemeters

Author(s): Young, R. P.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Report Number: AEDC TDR 62-58
full text available

The Effect Of Heat Release On The Flow Parameters In Shock-Induced Combustion

Author(s): Rhodes, R. P.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report Number: AEDC TDR 62-78
full text available

An Analysis of Nonequilibrium Inviscid Flow

Author(s): Gibson, W. E.
Corporate Author: Cornell Aeronautical, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report Number: AEDC TDR 62-172
full text available

Performance Of A Two-Stage Launcher Using Hydrogen

Author(s): Stephenson, W. B.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Report Number: AEDC TDR 62-32
full text available

A Two-Color Pyrometer for the Measurement of Temperature and Contamination Level in a Spark-Heated Hypervelocity Wind Tunnel

Author(s): Vali, Walter
Corporate Author: Stanford University
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report Number: AEDC TDR 62-174
full text available

Evaluation of a Gas Bearing Pivot for a High Amplitude Dynamic Stability Balance

Author(s): Hodapp, A. E., Jr.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-12
Report Number: AEDC TDR 62-221
full text available

Inductive Power Supply For A Hotshot-Type Tunnel

Author(s): Fillers, A. H., Jr.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report Number: AEDC TDR 62-137
full text available

A Pressure Data System For A 50-In. Continuous Mach 8 Wind Tunnel

Author(s): Hightower, F. C., Jr.
Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report Number: AEDC TDR 62-96
full text available

Tables of the Thermodynamic Properties of Nitrogen From 100 to 1500°K

Author(s): Little, Wanda J.
Corporate Author: ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-09
Report Number: AEDC TDR 62-170
full text available