Add to ORKGWind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of sweepback were made at low speeds to evaluate the effects of the nacelle on the aerodynamic characteristics of the wing. Force, moment, and pressure-distribution measurements are presented for the nacelle underslung and centrally mounted on the wing and mounted on a strut below the wing
Contains results of tunnel tests to determine effects of various combinations of split flaps, slats,...
As part of a propulsion/airframe integration program, tests were conducted in the Langley 16-Foot Tr...
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted ...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
A wing interference investigation was conducted to determine why the N.A.C.A. cowling did not yield ...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
Tests were made in the NACA 19-foot pressure tunnel of a simplified twin-engine bomber model with an...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
The arrow-wing transport configuration with detached engines located over the wing to produce upper ...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
An untwisted wing, which when unswept has an NACA 65-210 section, an aspect ratio of 9.0 and a taper...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
As part of a propulsion/airframe integration program at Langley Research Center, tests were conducte...
Contains results of tunnel tests to determine effects of various combinations of split flaps, slats,...
As part of a propulsion/airframe integration program, tests were conducted in the Langley 16-Foot Tr...
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted ...
Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of swee...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
A wing interference investigation was conducted to determine why the N.A.C.A. cowling did not yield ...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
Tests were made in the NACA 19-foot pressure tunnel of a simplified twin-engine bomber model with an...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
The arrow-wing transport configuration with detached engines located over the wing to produce upper ...
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...
An untwisted wing, which when unswept has an NACA 65-210 section, an aspect ratio of 9.0 and a taper...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
As part of a propulsion/airframe integration program at Langley Research Center, tests were conducte...
Contains results of tunnel tests to determine effects of various combinations of split flaps, slats,...
As part of a propulsion/airframe integration program, tests were conducted in the Langley 16-Foot Tr...
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted ...