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Serial/Series Title:
NACA Technical Notes
Collection:
National Advisory Committee for Aeronautics Collection
- Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers
- No Description digital.library.unt.edu/ark:/67531/metadc56152/
- Analysis of performance of a jet engine from characteristics of components II : interaction of components as determined from engine operation
- No Description digital.library.unt.edu/ark:/67531/metadc54905/
- Analysis of performance of jet engine from characteristics of components I : aerodynamic and matching characteristics of turbine component determined with cold air
- No Description digital.library.unt.edu/ark:/67531/metadc54255/
- Analysis of planing data for use in predicting hydrodynamic impact loads
- No Description digital.library.unt.edu/ark:/67531/metadc54792/
- Analysis of propeller efficiency losses associated with heated-air thermal de-icing
- No Description digital.library.unt.edu/ark:/67531/metadc54988/
- Analysis of pure-bending flutter of a cantilever swept wing and its relation to bending-torsion flutter
- No Description digital.library.unt.edu/ark:/67531/metadc55820/
- An Analysis of Ramjet Engines Using Supersonic Combustion
- No Description digital.library.unt.edu/ark:/67531/metadc57482/
- Analysis of shear strength of honeycomb cores for sandwich constructions
- No Description digital.library.unt.edu/ark:/67531/metadc55598/
- Analysis of shock motion in ducts during disturbances in downstream pressure
- No Description digital.library.unt.edu/ark:/67531/metadc56501/
- An analysis of shock-wave cancellation and reflection for porous walls which obey an exponential mass-flow pressure-difference relation
- No Description digital.library.unt.edu/ark:/67531/metadc57481/
- Analysis of square shear web above buckling load
- A solution of Von Karman's fundamental equations for plates with large deflections is presented for the case of a shear web divided into square panels by reinforcing struts. Numerical solutions are given for struts of infinite rigidity and for struts the weight of which is one-fourth the weight of the sheet. The results are compared with Wagner's diagonal tension theory as extended by Kuhn and by Langhaar. It is found that the diagonal tension theory as developed by Kuhn agrees best with the present paper in the practical range when r=1/4. Kuhn's theory is in especially good agreement for the force in the strut when r=1/4. digital.library.unt.edu/ark:/67531/metadc57287/
- Analysis of static aeroelastic behavior of low-aspect-ratio rectangular wings
- No Description digital.library.unt.edu/ark:/67531/metadc56318/
- An analysis of statically indeterminate trusses having members stressed beyond the proportional limit
- No Description digital.library.unt.edu/ark:/67531/metadc56905/
- Analysis of straight multicell wings on Cal-Tech analog computer
- No Description digital.library.unt.edu/ark:/67531/metadc57020/
- Analysis of stresses and deflections in a disk subjected to gyroscopic forces
- No Description digital.library.unt.edu/ark:/67531/metadc57165/
- Analysis of stresses in the plastic range around a circular hole in a plate subjected to uniaxial tension
- No Description digital.library.unt.edu/ark:/67531/metadc57768/
- An analysis of supersonic flow in the region of the leading edge of curved airfoils, including charts for determining surface-pressure gradient and shock-wave curvature
- No Description digital.library.unt.edu/ark:/67531/metadc56161/
- Analysis of sweptback wings on Cal-Tech analog computer
- No Description digital.library.unt.edu/ark:/67531/metadc57030/
- An analysis of the airspeed and normal accelerations of Douglas DC-2 airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc54947/
- An analysis of the airspeeds and normal accelerations of Boeing B-247 and B-247D airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc55049/
- An analysis of the airspeeds and normal accelerations of Boeing S-307 airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc55014/
- An analysis of the airspeeds and normal accelerations of Douglas DC-3 airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc55018/
- An analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc54787/
- An analysis of the airspeeds and normal accelerations of Sikorsky S-42A airplanes in commercial transport operation
- No Description digital.library.unt.edu/ark:/67531/metadc54995/
- An analysis of the compressive strength of honeycomb cores for sandwich construction
- No Description digital.library.unt.edu/ark:/67531/metadc55491/
- Analysis of the creep behavior of a square plate loaded in edge compression
- No Description digital.library.unt.edu/ark:/67531/metadc57275/
- An analysis of the effect of lift-drag ratio and stalling speed on landing-flare characteristics
- No Description digital.library.unt.edu/ark:/67531/metadc55245/
- An analysis of the effect of several parameters on the stability of an air-lubricated hydrostatic thrust bearing
- No Description digital.library.unt.edu/ark:/67531/metadc56526/
- An analysis of the errors in curve-fitting problems with an application to the calculation of stability parameters from flight data
- No Description digital.library.unt.edu/ark:/67531/metadc56284/
- An analysis of the factors affecting the loss in lift and shift in aerodynamic center produced by the distortion of a swept wing under aerodynamic load
- No Description digital.library.unt.edu/ark:/67531/metadc56557/
- An analysis of the factors affecting the state of fuel and air mixtures
- No Description digital.library.unt.edu/ark:/67531/metadc54826/
- An analysis of the factors that affect the exhaust process of a four-stroke-cycle reciprocating engine
- No Description digital.library.unt.edu/ark:/67531/metadc55117/
- Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber
- No Description digital.library.unt.edu/ark:/67531/metadc57748/
- An analysis of the main spray characteristics of some full-size multi-engined flying boats
- No Description digital.library.unt.edu/ark:/67531/metadc54869/
- An analysis of the normal accelerations and airspeeds of a four-engine airplane type in postwar commercial transport operations on trans-Pacific and Caribbean-South American routes
- No Description digital.library.unt.edu/ark:/67531/metadc55523/
- An analysis of the normal accelerations and airspeeds of a two-engine type of transport airplane in commercial operations on routes in the central United States from 1948 to 1950
- No Description digital.library.unt.edu/ark:/67531/metadc56288/
- An analysis of the optimization of a beam rider missile system
- No Description digital.library.unt.edu/ark:/67531/metadc56872/
- An analysis of the power-off landing maneuver in terms of the capabilities of the pilot and the aerodynamic characteristics of the airplane
- No Description digital.library.unt.edu/ark:/67531/metadc57347/
- An analysis of the stability and ultimate bending strength of multiweb beams with formed-channel webs
- No Description digital.library.unt.edu/ark:/67531/metadc57598/
- An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringer
- A method of strength analysis of short sheet-stringer panels subjected to compression is presented which takes into account the effect that the riveted attachments between the plate and the stiffeners have on the strength of the panels. An analysis of experimental data shows that panel strength is highly influenced by rivet pitch, diameter, and location and that the degree of influence for a given riveting depends on the panel configuration and panel material. (author). digital.library.unt.edu/ark:/67531/metadc57779/
- An analysis of the transition of a helicopter from hovering to steady autorotative vertical descent
- No Description digital.library.unt.edu/ark:/67531/metadc55233/
- An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection
- No Description digital.library.unt.edu/ark:/67531/metadc56733/
- Analysis of the ultimate strength and optimum proportions of multiweb wing structures
- No Description digital.library.unt.edu/ark:/67531/metadc57902/
- An analysis of the variation with altitude of effective gust velocity in convective-type clouds
- No Description digital.library.unt.edu/ark:/67531/metadc54711/
- An analysis of turbojet-engine-inlet matching
- A method of presenting turbojet-engine air-flow requirements and inlet-system air-flow capacities in identical though independent parametric terms is developed. The application of the air-flow representation technique to the analysis of engine-inlet matching conditions is demonstrated. Several examples are presented to illustrate the application of the method to the explicit determination of inlet geometric variations required to improve the power-plant performance of supersonic airplanes. digital.library.unt.edu/ark:/67531/metadc56793/
- Analysis of turbulent flow and heat transfer in noncircular passages
- No Description digital.library.unt.edu/ark:/67531/metadc57477/
- Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties
- No Description digital.library.unt.edu/ark:/67531/metadc57461/
- Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages
- No Description digital.library.unt.edu/ark:/67531/metadc56839/
- Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics
- No Description digital.library.unt.edu/ark:/67531/metadc57645/
- Analysis of wind-tunnel data on directional stability and control
- No Description digital.library.unt.edu/ark:/67531/metadc59650/