An experimental investigation was conducted to evaluate several concepts for braking and steering a vehicle equipped with an air cushion landing system (ACLS). The investigation made use of a modified airboat equipped with an ACLS. Braking concepts were characterized by the average deceleration of the vehicle. Reduced lobe flow and cavity venting braking concepts were evaluated in this program. The cavity venting braking concept demonstrated the best performance, producing decelerations on the test vehicle on the same order as moderate braking with conventional wheel brakes. Steering concepts were evaluated by recording the path taken while attempting to follow a prescribed maneuver. The steering concepts evaluated included using rudders on...
Unpowered automatic approaches and landings with a CV990 aircraft were conducted to study navigation...
Several concepts are developed for air cushion landing systems (ACLS) which have the potential for i...
An investigation was conducted at the Langley aircraft landing loads and traction facility to determ...
An investigation was made to determine the feasibility of an automatic braking system for arresting ...
An experimental study was conducted in order to determine the landing-impact behavior of a 0.3-scale...
Solutions to various landing problems were obtained through unconventional systems. The first, of th...
Research relative to tire tread, powered-wheel taxiing, air cushion landing systems, and crosswind l...
The results of tests to determine the effect of wheel brakes on the landing run of an airplane under...
The behavior of various antiskid systems was investigated under controlled conditions. Results from ...
To brake in minimum distance, the tire slip must be controlled to ride the peak of the mu-slip curve...
The braking and cornering response of a slip velocity controlled, pressure bias modulated aircraft a...
An experimental investigation was conducted to study the performance of an aircraft tire under cycli...
The braking performance of a nine-place, light, twin-engine airplane was evaluated on comparative gr...
The advantages to be gained from braking have not been ignored, and in the search for a suitable met...
During maximum braking the average ratio of drag-force friction coefficient developed by the antiski...
Unpowered automatic approaches and landings with a CV990 aircraft were conducted to study navigation...
Several concepts are developed for air cushion landing systems (ACLS) which have the potential for i...
An investigation was conducted at the Langley aircraft landing loads and traction facility to determ...
An investigation was made to determine the feasibility of an automatic braking system for arresting ...
An experimental study was conducted in order to determine the landing-impact behavior of a 0.3-scale...
Solutions to various landing problems were obtained through unconventional systems. The first, of th...
Research relative to tire tread, powered-wheel taxiing, air cushion landing systems, and crosswind l...
The results of tests to determine the effect of wheel brakes on the landing run of an airplane under...
The behavior of various antiskid systems was investigated under controlled conditions. Results from ...
To brake in minimum distance, the tire slip must be controlled to ride the peak of the mu-slip curve...
The braking and cornering response of a slip velocity controlled, pressure bias modulated aircraft a...
An experimental investigation was conducted to study the performance of an aircraft tire under cycli...
The braking performance of a nine-place, light, twin-engine airplane was evaluated on comparative gr...
The advantages to be gained from braking have not been ignored, and in the search for a suitable met...
During maximum braking the average ratio of drag-force friction coefficient developed by the antiski...
Unpowered automatic approaches and landings with a CV990 aircraft were conducted to study navigation...
Several concepts are developed for air cushion landing systems (ACLS) which have the potential for i...
An investigation was conducted at the Langley aircraft landing loads and traction facility to determ...