Flight investigation of the effects of Apollo heat-shield singularities on ablator performance
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material performance
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.
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material performance
Stress distribution at crack tip in tension field for plane stress-strain using plastic deformation theory
Perturbation solution to blunt body stagnation region flow of radiating gas with radiation heat transfer
Analytic continuation of Appell hypergeometric series into linear combination of four infinite series
Definitions of extremaloids in relation to optimal control problems and Lagrange problems based on Pontryagin principles
Hill method of secular perturbations and determination of zero-rank effects in nonsingular vectorial elements of motion of planets, comets, and satellites
Two variable expansion method applied to ordinary differential equation and two wave propagation problems, comparing results with matched asymptotic expansions and coordinate stretching methods
Planetary motion zero-rank effects numerical integration, using Hill secular perturbation method and trace of dyadics
Optimal trajectory and control approximate solution by asymptotic expansion, considering Mayer variational problem solution
Linear time-invariant system dependent on small parameter epsilon, deriving conditions for bounded-input bounded-state stability
Saturn 5 suboptimal continuous guidance design, eliminating discontinuous control encountered in SA-502 flight
Accurate approximative solution to differential equations of oscillatory problem with perturbing damping
Perturbation theory for fuel space trajectory optimization
Description of experiments undertaken to define the phase-resetting behavior of the circadian rhythm of pupal eclosion in populations of fruitflies. An attempt is made to determine how and why the resetting response depends on the duration of a standard perturbation as well as on the time at which it is given. Plotting a three-dimensional graph of the measured emergence centroids vs the stimulus variables, the data are found to spiral up around a vertical rotation axis. Using a computer, a smooth surface, called the resetting surface, which approximately fits the helicoidal cloud of data points, is obtained and is shown to be best described as a vertical corkscrew linking together tilted planes. This corkscrew feature of the resetting surface is taken to indicate that there is an isolated perturbation following which there is either no circadian rhythm of emergence in the steady state, or one of unpredictable phase. A hypothesis concerning the clock dynamics underlying the eclosion rhythm is briefly sketched which encompasses the main features of known resetting data using single discrete pulses of any perturbing agent.
Approximation of the eigenvalues of certain self-adjoint operators defined by a formal differential operator in a Hilbert space. In general, two problems are studied. The first is the problem of defining a suitable Hilbert space operator that has eigenvalues. The second problem concerns the finite difference operators to be used.
Collision of all bodies in a perturbed n-body problem is analyzed by an extension of the author's results for a perturbed two-body problem (1969). A procedure is set forth to prove that the absolute value of energy in a perturbed n-body system remains bounded until the moment of collision. It is shown that the characteristics of motion in both perturbed problems are basically the same.
A continuous time, single input-single output, linear, time-invariant, distributed feedback system F sup epsilon, containing a small delay of length epsilon in the loop, is considered. Conditions are given under which L2-stability and L2-instability of this feedback system can be deduced from those of the reduced model obtained by neglecting the delay. The two system models associated with F sup epsilon are the low-frequency model F and the high frequency model F. The condition for neglecting the small delay is the L2-stability of the family of high-frequency models, where epsilon or = 0 is sufficiently small. A lemma and a theorem are given. The lemma gives sharp Nyquist-type conditions for the L2-stability and L2-instability of the family of high frequency models for sufficiently small epsilon or = 0, while the Theorem gives explicit conditions under which the small delay may or may not be neglected.
Explore the source record for details and available documents.