UNT Libraries Government Documents Department - 5,157 Matching Results

Search Results

Primary view of Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems-Effect of Method of Positioning the Radar Antenna on the Speed of Response
Abramovitz, Marvin
August 13, 1952
Primary view of Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Method of Positioning the Radar Antenna on the Speed of Response
Abramovitz, Marvin
August 13, 1952
Primary view of Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Missile Configuration on the Speed of Response
Abramovitz, Marvin
January 19, 1953
Primary view of The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane
Abramovitz, Marvin & Van Dyke, Rudolph D., Jr.
December 17, 1954
Primary view of Theoretical Investigation of the Effects of the Artificial-Feel System on the Maneuvering Characteristics of the F-89 Airplane
Abramovitz, Marvin; Schmidt, Stanley F. & Belsley, Steven E.
December 31, 1952
Primary view of Investigation of the Use of a Stick Force Proportional to Pitching Acceleration for Normal-Acceleration Warning
Abramovitz, Marvin; Schmidt, Stanley F. & Van Dyke, Rudolph D., Jr.
August 14, 1953
Primary view of Investigation of internal film cooling of exhaust nozzle of a 1000-pound-thrust liquid-ammonia liquid-oxygen rocket
Abramson, Andrew E.
June 17, 1952
Primary view of Natural Icing of an Axial-Flow Turbojet Engine in Flight for a Single Icing Condition
Acker, Loren W.
August 12, 1948
Primary view of Preliminary Results of Natural Icing of an Axial-Flow Turbojet Engine
Acker, Loren W.
August 6, 1948
Primary view of Preliminary results of natural icing of an axial-flow turbojet engine
Acker, Loren W.
August 6, 1948
Primary view of Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine
Acker, Loren W. & Kleinknecht, Kenneth S.
April 7, 1949
Primary view of Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
Acker, Loren W. & Kleinknecht, Kenneth S.
May 25, 1950
Primary view of Flight Comparison of Performance and Cooling Characteristics of Exhaust-Ejector Installation with Exhaust-Collector-Ring Installation
Acker, Loren W. & Kleinknecht, Kenneth S.
February 14, 1947
Primary view of Accelerations in fighter-airplane crashes
Acker, Loren W.; Black, Dugald O. & Moser, Jacob C.
November 4, 1957
Primary view of Flying qualities of a high-performance personal-owner airplane
Adams, James J. & Whitten, James B.
November 8, 1951
Primary view of Tests of a centering spring used as an artificial feel device on the elevator of a fighter airplane
Adams, James J. & Whitten, James B.
September 12, 1952
Primary view of Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method
Adams, Richard E. & Silsby, Norman S.
April 11, 1947
Primary view of Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41
Adamson, D. & Boatright, William B.
September 14, 1950
Primary view of Effects of Combinations of Aspect Ratio and Sweepback at High Subsonic Mach Numbers
Adler, Alfred A.
June 4, 1947
Primary view of Horizontal-Tail Parameters as Determined From Flight-Test Tail Loads on a Flexible Swept-Wing Jet Bomber
Aiken, William S., Jr. & Fisher, Raymond A.
January 17, 1957
Primary view of Strain-Gage Measurements of Buffeting Loads on a Jet-Powered Bomber Airplane
Aiken, William S., Jr. & See, John A.
March 19, 1951
Primary view of Drag Measurements of a 34 Degree Swept-Forward and Swept-Back NACA 65-009 Airfoil of Aspect Ratio 2.7 as Determined by Flight Tests at Supersonic Speeds
Alexander, Sidney R.
February 20, 1947
Primary view of Drag Measurements of a Swept-Back Wing Having Inverse Taper as Determined by Flight Tests at Supersonic Speeds
Alexander, Sidney R.
April 8, 1947
Primary view of Drag Measurements of Symmetrical Circular-Arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
Alexander, Sidney R.
March 7, 1947
Back to Top of Screen