Experimental Measurements of the Effects of Airplane Motions on Wing and Tail Angles of Attack of a Swept-wing Bomber in Rough Air
Explore the source record for details and available documents.
Engel, Jerome N↗
SEARCH · Engineering Papers
Results for “Angle of attack”
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.
Wind-tunnel Investigation of External-flow Jet-augmented Double Slotted Flaps on a Rectangular Wing at an Angle of Attack of 0 Degree to High Momentum Coefficients
A wind-tunnel investigation has been made to determine the characteristics of external-flow jet-augmented double slotted flaps which appear suitable for application to airplanes with pod-mounted engines. The investigation included tests of the rectangular wing with an aspect ratio of 6 over a momentum-coefficient range from 0 to 28. Lift coefficients larger than the jet reaction in the lift direction were obtained with the external-flow jet-augmented double slotted flaps.
HIGH-LIFT DEVICES - COMPLETE WINGS↗
Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
Explore the source record for details and available documents.
Wiggins, James W↗
Experimental investigation of the lateral trim of a wing-propeller combination at angles of attack up to 90 degrees with all propellers turning in the same direction
Explore the source record for details and available documents.
Newsom, William A , Jr↗
Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll
Explore the source record for details and available documents.
Moul, Martin T↗
Summary of methods of measuring angle of attack on aircraft
Explore the source record for details and available documents.
Gracey, William↗
Preliminary Heat-transfer Studies on Two Bodies of Revolution at Angle of Attack at a Mach Number of 3.12
Explore the source record for details and available documents.
Sands, Norman↗
Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow
Explore the source record for details and available documents.
Brunk, William E↗
The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane
Explore the source record for details and available documents.
Gadeberg, Burnett L↗
Investigation at Supersonic Speed (M = 1.53) of the Pressure Distribution over a 63 Degrees Swept Airfoil of Biconvex Section at Several Angles of Attack
Explore the source record for details and available documents.
Katzen, Elliott D↗
An empirically derived method for calculating pressure distribution at supercritical Mach numbers and moderate angles of attack
Explore the source record for details and available documents.
Nitzberg, Gerald E↗
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds
Explore the source record for details and available documents.
Daley, Bernard N↗
Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack : subsonic speeds
Explore the source record for details and available documents.
Gracey, William↗
Flight investigation of a roll stabilized missile configuration at varying angles of attack at Mach numbers between 0.8 and 1.79
Explore the source record for details and available documents.
Zarovsky, Jacob↗
Aerodynamic characteristics of NACA RM 10 missile in 8 by 6 foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98. III : analysis of force distribution at angle of attack (stabilizing fins removed)
Explore the source record for details and available documents.
Luidens, Roger W↗
Static Longitudinal Stability and Dynamic Characteristics at High Angles of Attack and at Low Reynolds Numbers of a Model of the X-3 Supersonic Research Airplane
Explore the source record for details and available documents.
Burk, Sanger M↗
Subsonic Mach and Reynolds Number Effects on the Surface Pressures, Gap Flow, Pressure Recovery, and Drag of a Nonrotating NACA 1-series E-type Cowling at an Angle of Attack of 0 Degrees
Explore the source record for details and available documents.
Reynolds, Robert M↗
Wing-flow investigation of a 45 degrees cone as an angle-of-attack measuring device at transonic speeds
Explore the source record for details and available documents.
Mcclanahan, Herbert C , Jr↗