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Supplementary Bibliography of NACA Reports Related to Instrumentation and Research Techniques
Memorandum listing NACA reports related to a variety of research topics, including instruments, research equipment, and research techniques.
Date:
June 19, 1952
Creator:
The Division of Research Information
System:
The UNT Digital Library
Some Effects of Aeroelasticity at Mach Numbers From 0.7 to 1.6 on the Rolling Effectiveness of Thin Flat-Plate Delta Wings Having 45 Degree Swept Leading Edges and Full-Span Constant-Chord Ailerons
From Summary: "The aeroelastic effects on wing-aileron rolling effectiveness and drag of thin flat-plate delta wings with 45 degree swept leading edge and plain constant-chord ailerons have been investigated. This investigation has been carried out over a Mach number range of 0.7 to 1.6 by means of rocket-propelled test vehicles in free flight. The results show a near-linear decrease in lateral control effectiveness with a decrease in the wing torsional stiffness. An aileron-effectiveness reversal was experienced with the more flexible delta-wing models."
Date:
February 19, 1952
Creator:
Marley, Edward T. & English, Roland D.
System:
The UNT Digital Library
Longitudinal frequency-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements, including a method for the evaluation of transfer functions
Report presenting longitudinal frequency-response characteristics of a 35 degree swept-wing airplane computed from flight measurements. Also presented are pitching-velocity frequency responses to displacements of the adjustable stabilizer. Results regarding frequency-response curves, transfer functions, elevator effectiveness, altitude variations, and potential errors in data are provided.
Date:
September 19, 1951
Creator:
Triplett, William C. & Smith, G. Allan
System:
The UNT Digital Library