Search U.S. government technical reports digitized or harvested by TRAIL.
Design of nozzles for the individual cylinder exhaust jet propulsion system
Determination of control-surface characteristics from NACA plain-flap and tab data
Statistical analysis of the time and fatigue strength of aircraft wing structures
Tail-load measurements on the XB-15 bomber in gusty air
Effect of humidity on several supercharger parameters
The temperature of unheated bodies in a high-speed gas stream
Flight measurements of the elevator deflections used in landings of several airplanes
Normal-pressure tests of circular plates with clamped edges
Preliminary data on buckling strength of curved sheet panels in compression
Preliminary drag tests in flight of low-drag wing on the Curtiss XP-60 airplane
Present and future problems of airplane propulsion
Critical Compressive Stress for Outstanding Flanges
Design charts for cross-flow tubular intercoolers charge-across-tube type
Design charts for cross-flow tubular intercoolers charge-through-tube type
An analytical study of wing and tail loads associated with an elevator deflection
Air transport by gliders : some technical observations
Effect of propeller operation on the pitching moments of single-engine monoplanes
Experiences with flow-direction instruments
Preignition characteristics of several fuels under simulated engine conditions
Damping characteristics of dashpots
An apparatus for measuring rates of discharge of a fuel-injection system
Combined beam-column stresses of aluminum-alloy channel sections
The additional-mass effect of plates as determined by experiments
Some comparative tests of plain and alclad 24S-T sheet
Comparison of stress-strain curves obtained by single-thickness and pack methods
Compression tests of some 17S-T aluminum-alloy specimens of I cross section
The end-plate effect of a horizontal-tail surface on vertical tail surface
Model Tests of a Wing-Duct System for Auxiliary Air Supply
Some effects of rainfall on flight of airplanes and on instrument indications
Tests of a gust-alleviating wing in the gust tunnel
Spin Tests of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range
Methods of analyzing wind-tunnel data for dynamic flight conditions
Analysis of Ground Effect on the Lifting Airscrew
Analytical Determination of Control System Pulley-Axis Angles
Cooling Effects of an Airplane Equipped With an NACA Cowling and a Wing-Duct Cooling System