Aerodynamics Series

Contents: 4 Data Items with 0 ESDUpac and 0 VIEWpac programs. Data Item A2 77032 79025 87035

Title Wind Engineering Series: titles. Issue 4. Fluctuating loads and dynamic response of bodies and structures in fluid flows - background information. Fluctuating response of circular cylinders in small groups in fluid flow - discussion and guide to data available. Calculation methods for along-wind loading. Part 2. Response of line-like structures to atmospheric turbulence.

Aerodynamics Volume 12 Title: AERODYNAMIC HEATING AND HEAT TRANSFER - Aerodynamic heating and heat transfer. Contents: 7 Data Items with 0 ESDUpac and 0 VIEWpac programs. Data Item 69009 69010 69011 69012 AERO 00.02.05 AERO 00.03.26 AERO W.S.00.03.18

Title Heat balance for flight vehicles. Heat transfer by forced convection between a two-dimensional laminar boundary layer and a smooth flat plate, with application to wedges, cylinders and cones. Heat transfer by forced convection between a two-dimensional turbulent boundary layer and a smooth flat plate, with application to wedges, cylinders and cones. Effects of kinetic heating on equilibrium temperature of flight vehicles. Heat transfer under conditions of forced convection for the subsonic turbulent flow of gases in smooth straight ducts of constant cross section. Wall and average gas temperatures for subsonic turbulent flow with heat transfer in ducts of constant circular cross section. Aerodynamic heating: temperatures at a perfectly insulated surface neglecting radiation

Aerodynamics Volume 13 Title:WIND-TUNNEL CORRECTIONS - Wind-tunnel corrections. Contents:2 Data Items with 0 ESDUpac and 0 VIEWpac programs. Data Item 76028 80024

Title Lift-interference and blockage corrections for two-dimensional subsonic flow in ventilated and closed wind-tunnels. Blockage corrections for bluff bodies in confined flow.

Aerodynamics Volume SW Title: AERODYNAMICS SOFTWARE. Contents:3 Data Items with 27 ESDUpac and 5 VIEWpac programs. Data Item AEROSW 04013 00009

Title Aerodynamics Series - Software. ESDU Computer Programs. Part 1: Introduction. ESDUview user manual.

A0025 v1.0 A0107 v1.0 A7011 v2.1 A7012 v1.0 A7435 v1.0 A8123 v2.0 A8124 v1.0 A8310 v2.0 A8701 v1.1 A8705 v1.1 A8708 v1.2 A8724 v1.2 A8840 v3.0 A8947 v1.0 A9005 v1.1 A9020 v1.0 A9034 v4.0

A9128 v1.0

A9315 v1.1 A9438 v1.1 A9510 v1.2 A9625 v3.0 A9903 v1.0

Computer Program for prediction of aircraft lateral stability derivatives in sideslip at subsonic speeds. Computer program for estimation of trailing vortex drag factors for wings with part-span trailing-edge plain flaps. Lift-curve slope and aerodynamic centre position of wings in inviscid subsonic flow. Lift-curve slope and aerodynamic centre position of wings in inviscid supersonic flow. Subsonic lift-dependent drag due to the trailing vortex wake for wings without camber or twist. Program for calculation of lift and drag of two staggered lifting surfaces at low speeds. Drag of axisymmetric cowls at zero incidence for subsonic Mach numbers. Calculation of oscillatory aerodynamics data for slender bodies.

FORTRAN

Wing pitching moment at zero lift at subcritical Mach numbers. Increment in aerofoil profile drag due to the deployment of a single-slotted flap. Rudder sideforce, yawing moment and rolling moment control derivatives at low speeds. Low-speed drag coefficient increment at constant lift due to fullspan plain flaps. Yawing moment and rolling moment coefficients for plain ailerons at subsonic speeds. Calculation of in-plane force and moment derivatives for inclined propellers at low forward speeds. First resonance frequency for ventilated wind tunnels operating at subsonic speeds. Calculation of airframe-induced upwash at subsonic speeds. Calculation of normal force and pitching moment of forebodycylinder combinations at angles of attack up to 90 degrees and Mach numbers up to 5, including effects of conical boat-tailing. Simplified method for the prediction of aerofoil excrescence drag magnification factor for turbulent boundary layers at subcritical Mach numbers. Maximum lift coefficient of plain aerofoils and wings at subsonic speeds. Estimation of leading-edge suction distribution for plane thin wings at subsonic speeds Computer program for estimation of spanwise loading of wings with camber and twist in subsonic attached flow. Drag due to lift for non-planar swept wings up to high angle of attack at subsonic speeds. Generation of GUNACA 23-series of low-drag aerofoils (directed input version).

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A9931 v2.1 B9510 v1.0

B9903 v1.0 B9931 v2.0

Computer program for estimation of lift curve for wing-fuselage combinations with high- lift devices at low speeds. Computer program for estimation of spanwise loading of wings with camber and twist in subsonic attached flow. Lifting-surface theory. (With Appendix A: effect of plain flaps) Generation of GUNACA 23 series of low-drag aerofoils (screen prompt version). Computer program for estimation of spanwise position of peak loading.

FORTRAN FORTRAN

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