28 reports
Performance of a 40-mm Combustion-Heated Light Gas Gun Launcher
Author(s): Lord, M. E. Corporate Author: VKF, ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1960-10 Report Number: AEDC TN 60-176
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
Force Tests of Standard Hypervelocity Ballistic Models HB-1 and HB-2 at Mach 1.5 to 10
Author(s): Gray, J. Don Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1963-08 Report Number: AEDC TDR 63-137
Tables of Thermodynamic Properties of Argon from 100 to 3000°K
Author(s): Little, Wanda J. Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1964-04 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): Clark, E. L. Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1964-03 Report Number: AEDC TDR 64-25
Theoretical Base Pressure Analysis of Axisymmetric Ejectors Without Induced Flow
Author(s): Bauer, R. C. Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1964-01 Report Number: AEDC TDR 64-3
Missile Motion Sensitivity to Dynamic Stability Derivatives
Author(s): Langham, T. F. Corporate Author: ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1980-09-01 Report Number: AEDC TR 80-11
Mollier Diagram for Nitrogen
Author(s): Humphrey, R. L. Corporate Author: VKF, ARO, Inc. Laboratory: Arnold Engineering Development Center Date of Publication: 1960-05 Report Number: AEDC TN 60-83