Bodies of revolution having minimum total drag in hypersonic flow
Minimum drag bodies in hypersonic flow using calculus of variations
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Minimum drag bodies in hypersonic flow using calculus of variations
Evaluation of methods for implementing minimum fuel and attitude hold control mode for Apollo Applications Orbital Workshop
Minimum fuel attitude control of spacecraft by Pontryagin principle and extended steepest descent method
Solar modulating function form changes resulting in hysteresis near solar minimum
Superconducting flux-flow resistivity minimum in Pb-Tl alloy, discussing thermal dissipation associated with temperature gradients across moving fluxoid
Fast and slow neutron latitude variation at aircraft altitudes during solar minimum, noting environment effects on measurement
Dynamics, stability and approach to equilibrium of bounded one dimensional collisionless plasma representing minimum energy states with nonlinear Vlasov equation solutions
Asymptotic stability of discrete homogeneous linear minimum-variance estimation formulas
Thrust, bank angle and angle of attack of aircraft minimum fuel lateral turns at constant altitude and specified velocities
Frequency shifts of Lamb dip minimum in helium- neon laser, considering effects of discharge tube parameters and gas pressure
Closed form solution for minimum fuel constant thrust trajectories for vehicle transfer in vacuum between arbitrary boundary conditions
Ionospheric vertical columnar electron content at midlatitudes near solar cycle minimum based on Faraday rotation data from Explorer 22
Quasi-optimum control law for minimum-time bounded acceleration rendezvous in central force field using Friedland technique, with application to lunar flight
Minimum energy mission plan for manned exploration of Mars
Mathematical correlation of effects of gravity, size, boiled liquid, pressure, and configuration on peak and minimum boiling heat fluxes
Minimum energy control of class of electrically driven vehicles with application to lunar roving vehicles
Flight comparison of techniques for determining minimum flying speed for large, subsonic jet transport
Approximate analytical solution for minimum impulse transfer between circular orbit and given hyperbolic velocity vector at infinity