Effectiveness at Transonic Speeds of Flap-type Ailerons for Several Spanwise Locations on a 4-percent-thick Sweptback-wing--fuselage Model with and Without Tails
Explore the source record for details and available documents.
Hieser, Gerald↗
SEARCH · Engineering Papers
Results for “Location”
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 high-angle-of attack performance of a 14 degree ramp-type inlet in various circumferential body locations : Mach number range 1.5 to 2.0
Explore the source record for details and available documents.
Mitchell, Glenn A↗
Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane
Explore the source record for details and available documents.
Sjoberg, S A↗
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered wings at transonic speeds
Explore the source record for details and available documents.
Hammond, Alexander D↗
Transonic Investigation of Effects of Spanwise and Chordwise External Store Location and Body Contouring on Aerodynamic Characteristics of 45 Degree Sweptback Wing-body Configurations
Explore the source record for details and available documents.
Pearson, Albin O↗
Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : static lateral and directional stability; Mach numbers of 1.41 a
Explore the source record for details and available documents.
Spearman, M Leroy↗
Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing--body Model and Pressure-distribution Measurements on an Inboard Aileron
Explore the source record for details and available documents.
Runckel, Jack F↗
Ground Simulator Studies of a Small Side-located Controller in a Power Control System
Explore the source record for details and available documents.
Assadourian, Arthur↗
Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
Explore the source record for details and available documents.
Dryer, Murray↗
Effects of Vertical Location of the Wing and Horizontal Tail on the Static Lateral and Directional Stability of a Trapezoidal-wing Airplane Model at Mach Numbers of 1.41 and 2.01
Explore the source record for details and available documents.
Robinson, Ross B↗
Effects of Vertical Location of Wing and Horizontal Tail on the Aerodynamic Characteristics in Pitch at Mach Numbers from 0.60 to 1.40 of an Airplane Configuration with an Unswept Wing
Explore the source record for details and available documents.
Stivers, Louis S , Jr↗
Summary of locations, extents, and intensities of turbulent areas encountered during flight investigations of the jet stream from January 7, 1957 to April 28, 1957
Explore the source record for details and available documents.
Copp, Martin R↗
Pressure Recovery and Drag Characteristics of a Forward Located Circular Scoop Inlet as Determined from Flight Tests for Mach Numbers from 0.8 to 1.6
Explore the source record for details and available documents.
Merlet, Charles F↗
Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96
Explore the source record for details and available documents.
Jacobsen, Carl R↗
Summary of locations and extents of turbulent areas encountered during flight investigations of the jet stream from October 1953 to May 1954 and November 1954 to July 1955
Explore the source record for details and available documents.
Fetner, Mary W↗
Free-Spinning Wind-Tunnel Tests of a Low-Wing Monoplane with Systematic Changes in Wings and Tails IV : Effect of Center-of-Gravity Location
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independently ballasted so as to be interchangeable with no change in mass distribution. For each of the 24 resulting wing-tail combinations, observations were made of the steady spin for four control settings and of recoveries for five control manipulations. The results are presented in the form of charts comparing the spin characteristics. The tests are part of a general investigation being made in the NACA free-spinning tunnel to determine the effects of systematic changes in wing and tail arrangement upon the steady-spin and the recovery characteristics of a conventional low-wing monoplane for various load distributions.
Seidman, Oscar↗
Ground Effect on Downwash Angles and Wake Location
A theoretical study was made of the reduction in downwash and the upward displacement of the wake in the presence of the ground, and some verification of theory was obtained by means of air-flow measurements made with a ground-board and image-wing combination. Methods are given for estimating the effects and numerous examples are included to illustrate the nature of these effects and to show their order of magnitude.
Katzoff, S↗
The development of satisfactory flying qualities on the Douglas dive bomber, model SBD-1 through flight testing successive modifications in control-surface area, hinge-line location, and aerodynamic-balance nose shape
Explore the source record for details and available documents.
STALLING - DOUGLAS SBD-1↗