Add to ORKGAn analysis has been made by the NACA of the effects of heat and compressibility in the flow through the internal systems of aircraft. Equations and charts are developed whereby the flow characteristics at key stations in a typical internal system may be readily obtained
This report has been prepare in response to a request for information from an aircraft company. A ty...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Report presenting a method of graphical analysis that allows for the prediction of the thermal and a...
This report describes an investigation of the characteristics of flow in the air passages of aircraf...
An investigation has been made to determine efficient arrangements for an internal-flow system of an...
The method of determining the pressure distribution on the fuselage is described, with special atten...
An analysis has been made by the NACA of the effects of heat and compressibility in the flow through...
This report has been prepare in response to a request for information from an aircraft company. A ty...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Report presenting a method of graphical analysis that allows for the prediction of the thermal and a...
This report describes an investigation of the characteristics of flow in the air passages of aircraf...
An investigation has been made to determine efficient arrangements for an internal-flow system of an...
The method of determining the pressure distribution on the fuselage is described, with special atten...
An analysis has been made by the NACA of the effects of heat and compressibility in the flow through...
This report has been prepare in response to a request for information from an aircraft company. A ty...
A study of the data obtained in a flight investigation of an R-2800-21 engine in a P-47G airplane wa...
Report presenting a method of graphical analysis that allows for the prediction of the thermal and a...