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Force and Pressure Tests of an Agard Calibration Model B at a Mach Number of 8
Report Number: AEDC TN 60-34
Author(s): L. D. Kayser and C. R. Fitch
Corporate Author: VKF, ARO, Inc.
Publication Date: 7/1/1960
Pages: 39
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0239559
Photo Enhancement: Incomplete
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Mollier Diagram for Nitrogen
Report Number: AEDC TN 60-83
Author(s): R. L. Humphrey, W. J. Little, and L. A. Seeley
Corporate Author: VKF, ARO, Inc.
Laboratory: Arnold Engineering Development Center
Publication Date: 5/1/1960
Pages: 39
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0236935
Photo Enhancement: Not Needed
Abstract Text:
Thermodynamic data for nitrogen are presented in Mollier diagram form covering the temperature range of 30 K to 15,000 K and the density range of 10(-6) to 10(3) atmospheres
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Determination of Damping Derivitives From Free-Oscillation Tests of Non-Linear Systems Using Energy Relations
Report Number: AEDC TN 60-104
Author(s): C. J. Welsh, L. K. Ward, and G. R. Ahsmuhs
Corporate Author: VKF, ARO, Inc.
Publication Date: 6/1/1960
Pages: 29
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0239155
Photo Enhancement: Incomplete
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Pressure Distribution Tests of Several Sharp Leading Edge Wings, Bodies, and Body-Wing Combinations at Mach 5 and 8
Report Number: AEDC TN 60-173
Author(s): R. E. Randall, D.R. Bell, and J. L. Burk
Corporate Author: VKF, ARO, Inc.
Publication Date: 9/1/1960
Pages: 66
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0243457
Photo Enhancement: Incomplete
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Performance of a 40-mm Combustion-Heated Light Gas Gun Launcher
Report Number: AEDC TN 60-176
Author(s): M. E. Lord
Corporate Author: VKF, ARO, Inc.
Laboratory: Arnold Engineering Development Center
Publication Date: 10/1/1960
Pages: 26
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0244541
Photo Enhancement: Complete
Abstract Text:
Calculation methods and experimental results are presented for the performance of a 40-mm light gas model launcher using a mixture of helium, hydrogen and oxygen. The effect of charging pressure on peake pressure in the chamber is given and compared to closed chamber combusiton. Heat lossess from the chamber were measured during cooling in the closed chamber firings. The effect of incomplete combustion were estimated. Performance of the launcher is summarized as muzzle velocity as a function of maximum chamber pressure for various projectile weights. The velocity of a 40-gram (a cylindrical slug of minimum practical weight) projectile would be 14,000 ft/sec at the maximum chamber design pressure of 60,000 psi.
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The NTIS Order Number for this report is: AD244541
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Flow Properties of an Unyawed 10-Deg Cone for Gamma = 1.28 to 1.40 at Mach Numbers of 1.5 to 8
Report Number: AEDC TN 60-178
Author(s): W. T. Strike, Jr. and B. B. Norton, Jr.
Corporate Author: VKF, ARO, Inc.
Publication Date: 10/1/1960
Pages: 85
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0243828
Photo Enhancement: Not Needed
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Force Tests of an Agard Calibration Model B at M = 2.5 to 6.0
Report Number: AEDC TN 60-182
Author(s): Jack D. Coats
Corporate Author: VKF, ARO, Inc.
Publication Date: 10/1/1960
Pages: 30
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0244544
Photo Enhancement: Incomplete
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An Investigation of the Boundary-Layer Characteristics in the Test Section of a 40- By 40-Inch Supersonic Tunnel
Report Number: AEDC TN 60-189
Author(s): Jerry Jones
Corporate Author: VKF, ARO, Inc.
Publication Date: 10/1/1960
Pages: 23
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0245362
Photo Enhancement: Incomplete
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Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory
Report Number: AEDC TN 60-191
Author(s): J. Don Gray
Corporate Author: VKF, ARO, Inc.
Publication Date: 11/1/1960
Pages: 36
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0246085
Photo Enhancement: Not Needed
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The Design and Evaluation of a Transistorized Current Amplifier with a Bandwidth of DC to 100 KC
Report Number: AEDC TN 60-194
Author(s): W. M. Crouch
Corporate Author: VKF, ARO, Inc.
Publication Date: 10/1/1960
Pages: 27
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0245596
Photo Enhancement: Incomplete
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Development of Capacitance and Inductance Driven Hotshot Tunnels
Report Number: AEDC TN 60-222
Author(s): J. Lukasiewicz, W. G. Harris, R. Jackson, J. A. van der Bliek, and R. M. Miller
Corporate Author: VKF, ARO, Inc.
Publication Date: 1/1/1961
Pages: 85
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0249421
Photo Enhancement: Incomplete
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Hypervelocity Arc-Tunnel Instrumentation
Report Number: AEDC TN 60-227
Author(s): W. T. Earheart, Jr. and D. S. Bynum
Corporate Author: VKF, ARO, Inc.
Publication Date: 12/1/1960
Pages: 38
Contract: AF 40(600)-800
Project: None Given
Task: None Given
AD Number: AD0247564
Photo Enhancement: Incomplete
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