Add to ORKGThe text gives theoretical formulas from which is computed a table for the pressure of air on coming to rest from various speeds, such as those of aircraft and propeller blades. Pressure graphs are given for speeds from 1 cm. Sec. up to those of swift projectiles
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
This report gives the pressure distribution and resistance found by theory and experiment for simple...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
In Technical Report no. 247 of the National Advisory Committee for Aeronautics theoretical formulas ...
The text gives theoretical formulas from which is computed a table for the pressure of air on coming...
The question to be treated is: how high is the pressure in the bow wave caused by a body flying at s...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
The aerodynamic forces on bodies of arbitrary shape were investigated under conditions such that the...
The problem of the intake of air is treated for a missile flying at supersonic speeds and of changin...
This report deals with the pressure distribution over airfoils at high speeds, and describes an exte...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
Report describes the development of a suitable speed nozzle for the first few thousand airplanes mad...
The pressure distribution and resistance found by theory and experiment for simple quadrics fixed in...
Simultaneous air-jow photographs and premuredis-tributian measurement~were made of the N. A. C. A. 4...
Some of the problems considered in this report include: thermodynamics of surface friction, applicat...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
This report gives the pressure distribution and resistance found by theory and experiment for simple...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
In Technical Report no. 247 of the National Advisory Committee for Aeronautics theoretical formulas ...
The text gives theoretical formulas from which is computed a table for the pressure of air on coming...
The question to be treated is: how high is the pressure in the bow wave caused by a body flying at s...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
The aerodynamic forces on bodies of arbitrary shape were investigated under conditions such that the...
The problem of the intake of air is treated for a missile flying at supersonic speeds and of changin...
This report deals with the pressure distribution over airfoils at high speeds, and describes an exte...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
Report describes the development of a suitable speed nozzle for the first few thousand airplanes mad...
The pressure distribution and resistance found by theory and experiment for simple quadrics fixed in...
Simultaneous air-jow photographs and premuredis-tributian measurement~were made of the N. A. C. A. 4...
Some of the problems considered in this report include: thermodynamics of surface friction, applicat...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
This report gives the pressure distribution and resistance found by theory and experiment for simple...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...