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Flugmechanik
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keywords:("Flugmechanik")
2-Dimensional Smoke Tunnel Tests of a Fairchild Aircraft Division Wagner 1 B Model
82° Inclination Debris Cloud Revealed by Radar
A Calculation of the Profile Drag of Airfoils at Low Mach Numbers
Accelerations on 24-Hour Satellites and Low Order Longitude Terms in the Geopotential
Accurate and Efficient Vortex-Capturing for Rotor Blade Vortex Interaction
A Comparison of Cowell Vs Power Series Numerical Integration as Applied to Orbital Calculations
Acoustic Testing of a High-Tip-Speed Fan with Bypass-Duct Liners - Overview
A Critical Examination of the Equation for the Drag of the Karman Vortex Street
Activities of the Institute for Aerospace Studies of Toronto University
Activities Report of the French Aerospace and Research Industry
Additional Studies of the Effects of Deformation on the Aerodynamic Characteristics of a Sailwing
A Discussion of Orbital Workshop Orientation and Gravitational Effects
A Dynamic Analysis of Aeroplanes Encountering Vortex Wake Turbulence
AERO-Astrodynamics Considerations for the APOLLO Telescope Mount
Aerodynamic Analysis of a Low Density Hypersonic Shock-Wind Tunnel
Aerodynamic Characteristics, Including Effect of Body Shape, of a Mach 6 Aircraft Concept
Aerodynamic Characteristics of 0.187-Scale Model of a Target Missile at Mach 1.80 to 2.16
Aerodynamic Characteristics of a Flared Body with Blunt Nose
Aerodynamic Characteristics of a Helicopter Rotor Airfoil as Affected by Simulated Ballistic Damage
Aerodynamic Characteristics of Rectangular Plates in Hypersonic Flow of a Rarefied Gas
Aerodynamic Characteristics of Rotor Airfoils as Affected by Simulated Ballistic Damage
Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
Aerodynamic Data for Calculation of Eldo-a Stationary in-Flight Loads and Loading Distribution
Aerodynamic Effects of a Serrated Strip Near the Leading Edge of an Airfoil
Aerodynamic Flight-Test Results for the Adaptive Compliant Trailing Edge
Aerodynamic Heating Measurements on Hypersonic Flight Exoerunebt (HYFLEX) Vehicle
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters