Collection
Serial/Series Title
6 Matching Results
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6
Neon 18
None
Date:
October 22, 1953
Creator:
Gow, J. D. & Alvarez, L. W.
System:
The UNT Digital Library
Development of Hydrogen-Oxygen Recombiners. Progress Report
It is the purpose of this report to review our experience with recombiners under actual reactor operating conditions, and to discuss new developments in the field.
Date:
October 22, 1953
Creator:
Ransohoff, J.A. & Spiewak, I.
System:
The UNT Digital Library
The Effect of Thyroid Extract on Serum Lipoproteins and Serum Cholesterol
None
Date:
October 22, 1953
Creator:
Strisower, B.; Gofman, J. W.; Galioni, E. F.; Almada, A. A. & Simon, A.
System:
The UNT Digital Library
Examination of Recent Lateral-Stability-Derivative Data
"In the present paper attention is directed to the aerodynamic parameters, the so-called stability derivatives, that affect the lateral behavior of airplanes and missiles. The discussion is centered on three important quantities, the effective-dihedral derivative, the directional-stability derivative, and the damping-in-roll derivative. These quantities are considered for a large angle-of-attack range at subsonic speeds" (p. 1).
Date:
October 22, 1953
Creator:
Malvestuto, Frank S., Jr. & Kuhn, Richard E.
System:
The UNT Digital Library
An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver
From Introduction: "This report presents the initial study, the tracking performance of typical fighter airplanes with fixed gunsights. The types of airplanes tested afford two comparisons of particular interest: that between typical World War II and currently operational fighters of greatly increased speed and altitude, and that between conventional and irreversabile power-boosted controls with artificial feel, both installed on the same airframe."
Date:
October 22, 1953
Creator:
Rathert, George A., Jr.; Gadeberg, Burnett L. & Ziff, Howard L.
System:
The UNT Digital Library
Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5
Report discussing free-flight tests of normal-shock nose-inlet models with 1-series, parabolic, and conic cowling profiles in order to investigate the external drag characteristics at an angle of attack of 0 degrees. The testing occurred at a variety of Mach numbers, mass-flow ratios, and Reynolds numbers. Information about the effect of afterbody length, basic data, and effect of cowl shape is provided.
Date:
October 22, 1953
Creator:
Sears, R. I.; Merlet, C. F. & Putland, L. W.
System:
The UNT Digital Library