Simulator studies of jet reaction controls for use at high altitude
Explore the source record for details and available documents.
Stillwell, Wendell H↗
Engineering topics
Drake, Hubert M
Publications and source records attributed to Drake, Hubert M.
Operational problems of manned orbital vehicles
Explore the source record for details and available documents.
Drake, Hubert M↗
Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics
Explore the source record for details and available documents.
Williams, Walter C↗
Flight Measurements of Directional Stability to a Mach Number of 1.48 for an Airplane Tested with Three Different Vertical Tail Configurations
Explore the source record for details and available documents.
Drake, Hubert M↗
Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight
Explore the source record for details and available documents.
Drake, Hubert M↗
Loads experienced in flights of two swept-wing research airplanes in the angle-of-attack range of reduced stability
Explore the source record for details and available documents.
Robinson, Glenn H↗
Analysis of Longitudinal Stability and Trim of the Bell X-1 Airplane at a Lift Coefficient of 0.3 to Mach Numbers near 1.05
Explore the source record for details and available documents.
Drake, Hubert M↗
Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder
Explore the source record for details and available documents.
Drake, Hubert M↗
Elevator-stabilizer Effectiveness and Trim of the X-1 Airplane to a Mach Number of 1.06
Explore the source record for details and available documents.
Drake, Hubert M↗
Measurements of aileron effectiveness of Bell X-1 airplane up to a Mach number of 0.82
Explore the source record for details and available documents.
Drake, Hubert M↗
Measured characteristics of the Douglas D-558-1 airplane (BuAero No. 37971) in two landings
Explore the source record for details and available documents.
Drake, Hubert M↗
Free-flight-tunnel Tests of a Target-seeking Glide-bomb Model with Flicker Lateral Control
Explore the source record for details and available documents.
Mckinney, Marion O , Jr↗
Results obtained during accelerated transonic tests of the Bell XS-1 airplane in flights to a Mach number of 0.92
Results are presented of tests up to a Mach number of 0.92 at altitudes around 30,000 feet. The data obtained show that the airplane can be flown to this Mach number above 30,000 feet. Longitudinal trim changes have been experienced but the forces involved have been small. The elevator effectiveness decreased about one-half with increase of Mach number from 0.70 to 0.87. Buffeting has been experienced in level flight but it has been mild and the associated tail loads have been small. No aileron buzz or other flutter phenomena have been noted.
STABILITY, LONGITUDINAL - DYNAMIC↗
Flight Characteristics at Low Speed of Delta-wing Models
Explore the source record for details and available documents.
Mckinney, Marion O , Jr↗
Correlation of experimental and calculated effects of product of inertia on lateral stability
Explore the source record for details and available documents.
STABILITY, LATERAL↗
Investigation of Stability and Control Characteristics of an Airplane Model with Skewed Wing in the Langley Free-flight Tunnel
Explore the source record for details and available documents.
Campbell, John A↗
The Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-Flight Tunnel
Explore the source record for details and available documents.
AILERONS↗