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NACA Technical Reports (1)
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NACA Technical Notes
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The 6-foot-4-inch wind tunnel at the Washington Navy Yard
The 300 H.P. Benz Aircraft Engine
The 1350 F stress-rupture properties of two wrought alloys and three cast alloys
N.A.C.A. control position recorder
N.A.C.A. Langley field wind tunnel apparatusthe tilting manometer
N.A.C.A. recording air speed meter
Abnormal grain growth in M-252 and S-816 alloys
Abnormal grain growth in nickel-base heat-resistant alloys
Abnormal grain growth in S-816 alloy
Absolute coefficients and the graphical representation of airfoil characteristics
Absolute dimensions of Karman vortex motion
Accelerations and passenger harness loads measured in full-scale light-airplane crashes
Accelerations in transport-airplane crashes
Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow
The accuracy of the substitute-stringer approach for determining the bending frequencies of multistringer box beams
An accurate and rapid method for the design of supersonic nozzles
An accurate method of measuring the moments of inertia of airplanes
Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles
Acoustic analysis of ram-jet buzz
Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces
Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines
Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel
Adaptation of aeronautical engines to high altitude flying
Adaptor for measuring principal strains with Tuckerman strain gage
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