Aeronautics + Research
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Aeronautics + Research
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Aeronautics + Research
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Incoming Resources
- A deflection formula for single-span beams of constant section subjected to combined axial and transverse loads, by Walter E. Burke
- Energy loss, velocity distribution, and temperature distribution for a baffled cylinder model, by Maurice J. Brevoort
- A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design, by H.A. Soulé and James A. Hootman
- Principal effects of axial load on moment-distribution analysis of rigid structures, by Benjamin Wylie James
- The influence of impact velocity on the tensile characteristics of some aircraft metals and alloys, by Donald S. Clark
- Astronautics and aeronautics, a chronology, 1996-2000, authors, Marieke Lewis and Ryan Swanson ; project manager, Alice R. Buchalter
- Further measurements of normal accelerations on racing airplanes, by N.F. Scudder and H.W. Kirschbaum
- Spinning characteristics of wings, by M.J. Bamber and R.O. House, IV
- The aerodynamic characteristics of six commonly used airfoils over a large range of positive and negative angles of attack, by Raymond F. Anderson
- On the frontier, flight research at Dryden, 1946-1981, Richard P. Hallion
- Comparative tests of pitot-static tubes, by Kenneth G. Merriam and Ellis R. Spaulding
- Remarks on the elastic axis of shell wings, by Paul Kuhn
- Some elementary principles of shell stress analysis with notes on the use of the shear center, by Paul Kuhn
- The initial torsional stiffness of shells with interior webs, by Paul Kuhn
- Tank tests of a model of a flying-boat hull with a fluted bottom, by John R. Dawson
- The effect of the angle of afterbody keel on the water performance of a flying-boat hull model, by John M. Allison
- The variation in pressures in the cockpit of an airplane in flight, by Thomas Carroll and William H. McAvoy
- Circular motion of bodies of revolution, by Carl Kaplan
- The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinning balance, by M.J. Bamber and C.H. Zimmerman
- Effect of air-entry angle on performance of a 2-stroke-cycle compression-ignition engine, by Sherod L. Earle and Francis J. Dutee
- Tests of nacelle-propeller combinations in various positions with reference to wings, by Donald H. Wood, II
- A simplified method for the calculation of airfoil pressure distribution, by H. Julian Allen
- A study of the factors affecting the range of airplanes, by David Biermann
- Propeller tests to determine the effect of number of blades at two typical solidities, by E.P. Lesley
- Maximum forces applied by pilots to wheel-type controls, by William H. McAvoy
- Piloting technique for recovery from spins, by W.H. McAvoy
- Strength tests of thin-walled duralumin cylinders of elliptic section, by Eugene E. Lundquist and Walter F. Burke
- The aerodynamic drag of flying-boat hull models as measured in the N.A.C.A. 20-foot wind tunnel, by Edwin P. Hartman, I
- A preliminary determination of normal accelerations on racing airplanes, by N.F. Scudder and H.W. Kirschbaum
- Wind-tunnel tests of a cyclogiro rotor, by John B. Wheatley and Ray Windler
- Medical benefits from space research
- Vortex noise from rotating cylindrical rods, by E.Z. Stowell and A.F. Deming
- Spinning characteristics of wings, 25 percent stagger ; 0 degree decalage ; gap/chord 1.0, by M.J. Bamber, II
- Wind-tunnel tests of a wing with a trailing-edge auxiliary airfoil used as a flap, by Richard W. Noyes
- Some fundamental considerations in regard to the use of power in landing an airplane, by Walter S. Diehl
- Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle, by Fred E. Weick
- Full-scale tests of metal propellers at high tip speeds, by Donald H. Wood
- A preliminary investigation of boundary-layer transition along a flat plate with adverse pressure gradient, by Albert E. von Doenhoff
- Method of testing oxygen regulators, by Harcourt Sontag and E.L. Borlik
- A history of suction-type laminar-flow control with emphasis on flight research, by Albert L. Braslow
- A flight investigation to increase the safety of a light airplane, by P.A. Hunter and J.R. Vensel
- Full-scale force and pressure-distribution tests on a tapered U.S.A. 45 airfoil, by John F. Parsons
- Adaptor for measuring principal strains with Tuckerman strain gage, by A.E. McPherson
- Test of an adjustable pitch model propeller at four blade settings, by E.P. Lesley
- Tank tests of three models of flying-boat hulls of the pointed-step type with different angles of dead rise - N.A.C.A. model 35 series, by John R. Dawson
- Drag of prestone and oil radiators on the YO-31A airplane, by S.J. DeFrance
- Bending stresses due to torsion in cantilever box beams, by Paul Kuhn
- Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, Donald H. Wood
- Performance of axial-flow fan and compressor blades designed for high loadings, by Seymour M. Bogdonoff and L. Joseph Herrig
- Notes on the technique of landing airplanes equipped with wing flaps, by Melvin N. Gough
Outgoing Resources
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