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40 reports
Description of the E-1 Tunnel, GDF
Author(s): C. J. Schueler Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1953 Report Number: AEDC TN 53-19
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Digital Manometer Reader for the Arnold Engineering Development Center
Author(s): Henry T. Chapek Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1955 Report Number: AEDC TR 54-32
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Calibration of the Gas Dynamics Facility Tunnel with Supply Pressures up to 60 psia and Mach Numbers from 1.4 to 2.5
Author(s): Charles E. Bond Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1955 Report Number: AEDC TN 54-45
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Influence of Plenum-chamber Suction and Wall Convergence on the Mach Number Distribution in Patially Open Test Sections of Wind Tunnels at Subsonic and Supersonic Speeds
Author(s): Bernhard H. Goethert Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 4/1/1955 Report Number: AEDC TR 54-42
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Tests of 6-inch Hydraulic Relief Valve with Amplifier Ring
Author(s): James M. Langford Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1955 Report Number: AEDC TN 54-29
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On-Line Automatic Data Reduction Tunnel E-1 Gas Dynamics Facility
Author(s): C. L. Hall; R. E. Klautsch Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 4/1/1956 Report Number: AEDC TN 56-4
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Performance of a 40-mm Combustion-Heated Light Gas Gun Launcher
Author(s): M. E. Lord Corporate Author: VKF, ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 10/1/1960 Report Number: AEDC TN 60-176
Mollier Diagram for Nitrogen
Author(s): R. L. Humphrey, W. J. Little, and L. A. Seeley Corporate Author: VKF, ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 5/1/1960 Report Number: AEDC TN 60-83
Performance Of A Two-Stage Launcher Using Hydrogen
Author(s): W. B. Stephenson and R. E. Knapp Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 3/1/1962 Report Number: AEDC TDR 62-32
An Examination Of Epoxy Systems Useful In Packaging High G Radio Telemeters
Author(s): R. P. Young Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 3/1/1962 Report Number: AEDC TDR 62-58
A Device for Measuring Heat Transfer Rates in Arc-Discharge Hypervelocity Wind Tunnels
Author(s): R. L. Ledford Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 5/1/1962 Report Number: AEDC TDR 62-64
The Effect Of Heat Release On The Flow Parameters In Shock-Induced Combustion
Author(s): R. P. Rhodes, P. M. Rubins, and D. E. Chriss Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 5/1/1962 Report Number: AEDC TDR 62-78
Experience With An Overexpanded Nozzle In A Low-Density, Hypervelocity Wind Tunnel
Author(s): J. Leith Potter and David E. Boylan Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 4/1/1962 Report Number: AEDC TDR 62-85
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A Pressure Data System For A 50-In. Continuous Mach 8 Wind Tunnel
Author(s): F. C. Hightower, Jr. Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 5/1/1962 Report Number: AEDC TDR 62-96
Source Flow Effects In Conical Hypervelocity Nozzles
Author(s): Jack D. Whitfield and Glenn D. Norfleet Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 6/1/1962 Report Number: AEDC TDR 62-116
Compensation Of Dynamic Sting Effects In Hotshot Force Measurements
Author(s): E. E. Edenfield and R. L. Ledford Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 6/1/1962 Report Number: AEDC TDR 62-122
Flow Characteristics Of A 40-Inch Wind Tunnel At Mach Numbers 1.5 To 6
Author(s): Jack D. Coats Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 6/1/1962 Report Number: AEDC TDR 62-130
Inductive Power Supply For A Hotshot-Type Tunnel
Author(s): A. H. Fillers, Jr. Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 7/1/1962 Report Number: AEDC TDR 62-137
Radio Telemetry of Stagnation Pressure from a wind Tunnel Model Magnetically Supported in Supersonic Flow,
Author(s): P. L. Clemens Corporate Author: Arnold Engineering Development Center Arnold Air Force Station Tenn Laboratory: Arnold Engineering Development Center Date of Publication: 7/1/1962 Report Number: AEDC TDR 62-141
Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow
Author(s): J. Leith Potter and John T. Miller Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 8/1/1962 Report Number: AEDC TDR 62-155
Fatigue Tests and Crack Detection on Some Types of Axial-Flow Compressor Rotor Blades
Author(s): R. E. Thomas Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 10/1/1962 Report Number: AEDC TDR 62-168
Tables of the Thermodynamic Properties of Nitrogen From 100 to 1500 Degrees K
Author(s): Wanda J. Little and C. A. Neel Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 9/1/1962 Report Number: AEDC TDR 62-170
An Analysis of Nonequilibrium Inviscid Flow
Author(s): W. E. Gibson and A. Sowydra Corporate Author: Cornell Aeronautical, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 8/1/1962 Report Number: AEDC TDR 62-172
A Two-Color Pyrometer for the Measurement of Temperature and Contamination Level in a Spark-Heated Hypervelocity Wind Tunnel
Author(s): Walter Vali and R. Stephen de Voto Corporate Author: Stanford University Laboratory: Arnold Engineering Development Center Date of Publication: 8/1/1962 Report Number: AEDC TDR 62-174
Addendum to an Investigation of the Equilibrium Pressure Along Unequally Heated Tubes
Author(s): G. D. Arney, Jr., and A. B. Bailey Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 10/1/1962 Report Number: AEDC TDR 62-188
The Drag of Spheres in Rarefied Hypervelocity Flow
Author(s): Max Kinslow and J. L. Potter Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 12/1/1962 Report Number: AEDC TDR 62-205
Further Experiments on Impact-Pressure Probes in a Low-Density, Hypervelocity Flow
Author(s): A. B. Bailey Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 11/1/1962 Report Number: AEDC TDR 62-208
Measurements of Pressure and Speed of Flow in a Spark-Heated Hypersonic Wind Tunnel
Author(s): Krishnamurty Karamcheti, Walter Vali, James B. Kyser, and Maurice L. Rasmussen Corporate Author: Stanford University Laboratory: Arnold Engineering Development Center Date of Publication: 11/1/1962 Report Number: AEDC TDR 62-218
Microwave Measurement of Projectile Kinematics Within Launcher Barrels
Author(s): R. E. Hendrix Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 11/1/1962 Report Number: AEDC TDR 62-213
Evaluation of a Gas Bearing Pivot for a High Amplitude Dynamic Stability Balance
Author(s): A. E. Hodapp, Jr. Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 12/1/1962 Report Number: AEDC TDR 62-221
Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles
Author(s): J. R. Henson; J. E. Robertson Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 5/1/1962 Report Number: AEDC TDR 62-7
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Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source
Author(s): C. T. Carman Corporate Author: Arnold Engineering Development Center Laboratory: Arnold Engineering Development Center Date of Publication: 3/1/1962 Report Number: AEDC TDR 62-15
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Inviscid and Viscous Hypersonic Nozzle Flow with Finite Rate Chemical Reactions
Author(s): E. S. Levinsky and J. J. Brainerd Corporate Author: General Dynamics/Astronautics Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1963 Report Number: AEDC TDR 63-18
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Force Tests of Standard Hypervelocity Ballistic Models HB-1 and HB-2 at Mach 1.5 to 10
Author(s): J. Don Gray; E. Earl Lindsay Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 8/1/1963 Report Number: AEDC TDR 63-137
Tables of Thermodynamic Properties of Argon from 100 to 3000 Degrees K
Author(s): Wanda J. Little Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 4/1/1964 Report Number: AEDC TDR 64-68
Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory
Author(s): E. L. Clark and L. L. Trimmer Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 3/1/1964 Report Number: AEDC TDR 64-25
Theoretical Base Pressure Analysis of Axisymmetric Ejectors Without Induced Flow
Author(s): R. C. Bauer Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1/1/1964 Report Number: AEDC TDR 64-3
Flow-Field Investigation of a 0.0667-Scale Model of the X-15 Research Vehicle at Mach 4, 6, 8
Author(s): J. Rippey Corporate Author: ARO, inc. Laboratory: Arnold Engineering Development Center Date of Publication: 10/1/1964 Report Number: AEDC -TDR-201
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Missile Motion Sensitivity to Dynamic Stability Derivatives
Author(s): T. F. Langham Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 9/1/1980 Report Number: AEDC TR 80-11
Numerical Solution of the Three-Dimensional Unsteady Euler Equations
Author(s): K. Koeing; J. M. Barton Corporate Author: Mississippi State University; Sverdrup Technology, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 8/1/1983 Report Number: AEDC TR 83-22
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