A detailed table of the standard equilibrium velocity and standard equilibrium time is presented for bodies falling in the standard atmosphere. This table gives the velocity at various altitudes and the time of fall from sea level to -4000 feet and from 80,000 feet to sea level. In addition to this standard table, there are given short tables and charts of an open-parachute descent and free-falls; the terminal velocity at sea level, and the variation of the weight-to-drag ratio (2w/cds)1/2 for various weight jumpers from 90 to 30 feet in open-parachute descent; and estimations of drag coefficients of silk and nylon parachutes. The table of standard equilibrium velocities and standard equilibrium times may be used directly for open-parachute...
A three-dimensional code in body-fitted coordinates was developed using MacCormack's algorithm. The ...
Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of ...
To obtain the absolute velocity of an airship by knowing the speed at which two routes are covered, ...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
The present report deals with temperature measurements on cylinders of 0.2 to 3 millimeters diameter...
At high latitudes, dispersions in values of density for the middle atmosphere from the Global Refere...
The resistance coefficients of commercial types of round wire grids were examined for the purpose of...
Following the description of the new propulsion system and the definition of the propulsive efficien...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
A procedure which takes into account the aerodynamic span effect is given for the determination of t...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
The most important factors in evaluating performance of gliders are minimum sinking speed and minimu...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
A detailed table of the standard equilibrium velocity and standard equilibrium time is presented for...
A three-dimensional code in body-fitted coordinates was developed using MacCormack's algorithm. The ...
Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of ...
To obtain the absolute velocity of an airship by knowing the speed at which two routes are covered, ...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
The present report deals with temperature measurements on cylinders of 0.2 to 3 millimeters diameter...
At high latitudes, dispersions in values of density for the middle atmosphere from the Global Refere...
The resistance coefficients of commercial types of round wire grids were examined for the purpose of...
Following the description of the new propulsion system and the definition of the propulsive efficien...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
A procedure which takes into account the aerodynamic span effect is given for the determination of t...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
The most important factors in evaluating performance of gliders are minimum sinking speed and minimu...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
A detailed table of the standard equilibrium velocity and standard equilibrium time is presented for...
A three-dimensional code in body-fitted coordinates was developed using MacCormack's algorithm. The ...
Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of ...
To obtain the absolute velocity of an airship by knowing the speed at which two routes are covered, ...