Re-entry Flight Demonstration Number Two: Interim Flight-Test Report (open access)

Re-entry Flight Demonstration Number Two: Interim Flight-Test Report

Abstract: This report presents a summary and brief evaluation of the RFD-2 flight-test data reduced as of December 16, 1964.
Date: January 8, 1965
Creator: Cropp, L. O.; Everhart, W. H.; Keck, L. J.; Klett, R. D.; Robertson, M. M.; Spahr, H. R. et al.
Object Type: Report
System: The UNT Digital Library
Final Report on Re-entry Flight Demonstration Number Two (open access)

Final Report on Re-entry Flight Demonstration Number Two

Abstract: RFD-2 was the second of Sandia's operational safety flight tests of systems for nuclear auxiliary power.
Date: April 8, 1965
Creator: Hansen, H. E.; Clark, A. J. & Bentz, A. E.
Object Type: Report
System: The UNT Digital Library

Hydrogeochemical and Stream Sediment Reconnaissance Basic Data for Plainview NTMS Quadrangle, Texas: Appendix D

From abstract: Results of a reconnaissance geochemical survey of the Plainview Quadrangle, Texas are reported. Field and laboratory data are presented for 969 groundwater samples and 571 stream sediment samples. Statistical and areal distributions of uranium and other possible uranium related variables are displayed. A generalized geologic map of the survey area is provided, and pertinent geologic factors which may be of significance in evaluating the potential for uranium mineralization are briefly discussed.
Date: June 8, 1978
Creator: National Uranium Resource Evaluation Program
Object Type: Dataset
System: The UNT Digital Library
An Investigation of the Characteristics of an Unswept Wing of Aspect Ratio 4.01 in the Langley 8-Foot High-Speed Tunnel (open access)

An Investigation of the Characteristics of an Unswept Wing of Aspect Ratio 4.01 in the Langley 8-Foot High-Speed Tunnel

Report presenting an investigation of the characteristics of a low-aspect-ratio wing at high subsonic Mach numbers in the high-speed tunnel. The wing model had an NACA 65-108 airfoil section, an aspect ratio of 4.01, a taper ratio of 0.498, and no twist or dihedral. Results regarding normal-force characteristics, pitching-moment characteristics, and drag characteristics are provided.
Date: November 8, 1949
Creator: Bielat, Ralph P. & Cahn, Maurice S.
Object Type: Report
System: The UNT Digital Library