Analysis of the effects of boundary-layer control on the power-off landing performance characteristics of a liaison type of airplane
Explore the source record for details and available documents.
Horton, Elmer A↗
SEARCH · Search NASA
Results for “BOUNDARY LAYER CONTROL - SUCTION - SLOTS”
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.
Investigation of the Effectiveness of Boundary-layer Control by Blowing over a Combination of Sliding and Plain Flaps in Deflecting a Propeller Slipstream Downward for Vertical Take-off
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over the flaps of a wing equipped with a 50-percent-chord sliding flap and a 25-percent-chord plain flap in deflecting a propeller slipstream downward for vertical take-off and the results are presented herein. The effects of a leading-edge slat, ground proximity, end plate, and propeller position were also investigated. The tests were conducted in a static-thrust facility at the Langley Aeronautical Laboratory.
AIRPLANES - PERFORMANCE↗
Investigation of the Effects of Propeller Diameter on the Ability of a Flapped Wing, with and Without Boundary-layer Control, to Deflect a Propeller Slipstream Downward for Vertical Take-off
Explore the source record for details and available documents.
Spreemann, Kenneth P↗
Effects of Boundary-layer Control on the Longitudinal Characteristics of a 45 Degrees Swept-forward Wing-fuselage Combination
Explore the source record for details and available documents.
Mccormack, Gerald M↗
Some Low-speed Characteristics of an Air-induction System Having Scoop-type Inlets with Provisions for Boundary-layer Control
Explore the source record for details and available documents.
Watson, Earl C↗
Performance of a Normal-shock Scoop Inlet with Boundary-layer Control
Explore the source record for details and available documents.
Frazer, Alson C↗
Preliminary Investigation of Some Internal Boundary-layer-control Systems on a Side Inlet at Mach Number 2.96
Explore the source record for details and available documents.
Piercy, Thomas G↗
Investigation of two short annular diffuser configurations utilizing section and injection as a means of boundary-layer control
Explore the source record for details and available documents.
Wilbur, Langley W↗
Preliminary analysis of performance of turbojet engines used as pumps for boundary-layer control
Explore the source record for details and available documents.
Conrad, E William↗
A wind-tunnel investigation of a 0.4 scale model of an assault-transport airplane with boundary-layer control applied
Explore the source record for details and available documents.
Fink, Marvin P↗
A Flight Evaluation of a Wing-shroud-blowing Boundary-layer Control System Applied to the Flaps of an F9F-4 Airplane
Explore the source record for details and available documents.
Rolls, L Stewart↗
Effects of Internal Boundary-layer Control on the Performance of Supersonic Aft Inlets
Explore the source record for details and available documents.
Obery, Leonard J↗
Effect of Boundary-layer Control and Inlet Lip Shape on the Performance of a Twin-scoop Air-induction System at Mach Numbers from 0 to 1.9
Explore the source record for details and available documents.
LAZZERONI FRANK A↗
Analysis of some parameters used in correlating blowing-type boundary-layer control data
Explore the source record for details and available documents.
Kelly, Mark W↗
Wind-tunnel Tests of Blowing Boundary-layer Control with Jet Pressure Ratios up to 9.5 on the Trailing-edge Flaps of a 35 Degree Sweptback Wing Airplane
Explore the source record for details and available documents.
Kelly, Mark W↗
Flight Measurements of the Low-speed Characteristics of a 35 Degree Swept-wing Airplane with Blowing-type Boundary-layer Control on the Trailing-edge Flaps
Explore the source record for details and available documents.
Anderson, Seth B↗
Effects of Internal-area Distribution, Spike Translation, and Throat Boundary-layer Control on Performance of a Double-cone Axisymmetric Inlet at Mach Numbers from 3.0 to 2.0
Explore the source record for details and available documents.
Conners, James F↗
Flight Investigation of the Low-speed Characteristics of a 45 Degree Swept-wing Fighter-type Airplane with Blowing Boundary-layer Control Applied to the Trailing Edge Flaps
Explore the source record for details and available documents.
Quigley, Hervey C↗