The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel with and Without Nacelles at Mach Numbers from 0.30 to 0.86
Explore the source record for details and available documents.
SEARCH · Search NASA
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.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Abstract not provided.
Abstract not provided.
Abstract not provided.
Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
Origin & distribution of supersonic store interference/measurement of individual forces - swept-wing heavy bomber with large store figure
Transonic performance of three turbojet nozzle- afterbody configurations
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Static longitudinal stability and control at angles of attack above those for wing stall in large-scale subsonic transport model
Wind tunnel study of aerodynamic interference drag caused by fan jet engine wake of subsonic transport
Low noise turbofan engine without aerodynamic blade loading
Modifications to reduce fan-compressor noise level of DC-8 aircraft - Part 2
Modifications to reduce fan-compressor noise level of DC-8 aircraft - Part 1
Static tests to determine effects of throat inlet concepts on forward-radiated fan noise of 707-320B/C airplanes