Incoming Resources
- Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63, by Odell A. Morris and Robert J. Mack
- The use of demand-to-capacity indexes for the iterative design of rigid structures for wind, Filmon Habte, Arindam Gan Chowdhury, Sejun Park
- Time-accurate numerical prediction of free flight aerodynamics of a finned projectile, Jubaraj Sahu
- Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds, by John C. Martin and Frank S. Malvestuto, Jr
- Shock waves and drag in the numerical calculation of isentropic transonic flow, by Joseph L. Steger and Barrett S. Baldwin
- Development of a laser-induced heat flux technique for measurement of convective heat transfer coefficients in a supersonic flowfield, by A. Robert Porro
- Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8, by W.F. Lindsey, D.B. Stevenson, and Bernard N. Daley
- Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation, by Russell B. Sorrells and David S. Miller
- Improvement of aileron effectiveness by the prevention of air leakage through the hinge gap as determined in flight, by H.A. Soulé and W. Gracey
- The N.A.C.A. CYH airfoil section, by George J. Higgins
- Design of a slotted, natural-laminar-flow airfoil for business-jet applications, Dan M. Somers
- Dual methods and approximation concepts in structural synthesis, Claude Fleury and Lucien A. Schmit, Jr
- An experimental evaluation of the performance of two combination pitot pressure probes, David J. Arend and John D. Saunders ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
- Note on the air forces on a wing caused by pitching, by Max M. Munk
- An entropy correction method for unsteady full potential flows with strong shocks, Woodrow Wilson, Jr., Mohamed M. Hafez, Stanley J. Osher
- Hypersonic aerodynamic characteristics of a model of low-fineness-ratio variable-geometry logistics spacecraft concept, by Bernard Spencer
- Exploding wire initiation and electrical operation of a 40-kV system for arc-heated drivers up to 10 feet long, by Robert E. Dannenberg and Anthony F. Silva
- The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage, reported by M.F. Blair
- Prediction of turbulent diffusing flows using FUN3D, David J. Friedlander, Julianne C. Dudek, and May-Fun Liou
- Rotating rig development for droplet deformation/breakup and impact induced by aerodynamic surfaces, A. Feo, M. Vargas, A Sor
- Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor, Kevin Wilkes and Walter F. O'Brien, A. Karl Owen
- Coupled CFD/GN&C modeling for a smart material canard actuator, Paul Weinacht
- Identification of best practices for predicting inlet performance using FUN3D part 2, installed inlets, Michael D. Bozeman Jr. and Jan-Renee Carlson
- Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV, David F. Fisher, Daniel G. Murri, and Wendy R. Lanser
- Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86, by Cornelius Driver
- A direct-fire trajectory model for supersonic, transonic, and subsonic projectile flight, Paul Weinacht
- Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections, by Laurence K. Loftin, Jr. and Kenneth S. Cohen
- Leading-edge deflection optimization for a highly swept arrow-wing configuration, Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert
- Hypersonic airbreathing propulsion, an aerodynamics, aerothermodynamics, and acoustics competency white paper, J. Philip Drummond [and eleven others]
- Notes on aerodynamic forces, by Max M. Munk, III
- A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications, Rickey J. Shyne
- Precision of wing sections and consequent aerodynamic effects, by Frank Rizzo
- Aerodynamics of slender wings and wing-body combinations having swept trailing edges, by Harold Mirels
- Experimental stagnation-point velocity gradients and heat-transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack, by James C. Ellison
- Conceptual design approach for small-caliber aeroballistics with application to 5.56-mm ammunition, by Paul Weinacht, James F. Newill, and Paul J. Conroy
- CFD prediction of Magnus effect in subsonic to supersonic flight, by James DeSpirito
- The Caproni seaplane, by Max Munk
- Transonic aerodynamic characteristics of two hypersonic cruise configurations, by Richard A. Langhans
- Flow through very porous screens, Paul A. Durbin and Kenneth K. Muramoto
- Heat-transfer and pressure distributions on spherically blunted 25° half-angle cone at Mach 8 and angles of attack up to 90°, by Dennis M. Bushnell, Robert A. Jones, and Jarrett K. Huffman
- Flight investigation of the effects of Apollo heat-shield singularities on ablator performance, by Thomas E. Walton, Jr., William G. Witte, and Brian J. O'Hare
- View factors for toroids and their parts, by Norman T. Grier and Ralph D. Sommers
- Subsonic dynamics of stardust sample return capsule, R.A. Mitcheltree and C.M. Fremaux
- Validation of the gas generator method of calculating jet-engine thrust and evaluation of XB-70-1 airplane engine performance at ground static conditions, by Henry H. Arnaiz and William G. Schweikhard
- The increase in frictional resistance caused by various types of rivet heads as determined by tests of planing surfaces, by Starr Truscott and J.B. Parkinson
- Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶, by Laurence K. Loftin, Jr
- The induction factor used for computing the rolling moment due to the ailerons, by Max M. Munk
- Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range, David W. Bogdanoff
- Aerodynamic properties of slender wing-body combinations at subsonic, transonic, and supersonic speeds, by John R. Spreiter
- Supersonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle, George M. Ware and Walter C. Engelund, Ian O. MacConochie