National Advisory Committee for Aeronautics (NACA) - 20 Matching Results

Search Results

Results: 1 - 20
Primary view of An Analysis of Airspeeds and Mach Numbers Attained by Lockheed Constellation Airplanes in Transcontinental Operations During the Early Summer of 1946
Steiner, Roy
October 10, 1947
Primary view of Analytical Comparison of a Standard Turbojet Engine, a Turbojet Engine with a Tail-Pipe Burner, and a Ram-Jet Engine
Krebs, Richard P. & Palasics, John
February 10, 1947
Primary view of Ditching Tests of a 1/18-Scale Model of the Navy XP4M-1 Airplane in Langley Tank No. 2 and on an Outdoor Catapult, TED No. NACA 2362
Fisher, Lloyd J. & Hoffman, Edward L.
March 10, 1947
Primary view of Effect of Air-Flow Distribution and Total-Pressure Loss on Performance of One-Sixth Segment of Turbojet Combuster
Hill, Francis U. & Mark, Herman
December 10, 1947
Primary view of Effect of Chordwise Vanes on Amplitude of Tail Buffeting
Stokke, Allen R.
November 10, 1947
Primary view of The Effect of Sample Size on the Determination of Maximum Gust Velocities in Clouds
Press, Harry
October 10, 1947
Primary view of Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000
Salmi, Reino J.; Conner, D. William & Graham, Robert R.
June 10, 1947
Primary view of Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 22, 1946 to July 23, 1946 at Orlando, Florida
Tolefson, H. B.
March 10, 1947
Primary view of Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Static Longitudinal Stability of Models with Wing Flap Deflections of 0 Deg and 15 Deg, TED No. NACA 2387
Stone, David G.
January 10, 1947
Primary view of The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions
Allen, H. Julian; Heaslet, Max A. & Nitzberg, Gerald E.
April 10, 1947
Primary view of The interdependence of various types of autoignition and knock
Olsen, H. Lowell & Miller, Cearcy D.
February 10, 1947
Primary view of Interference Method for Obtaining the Potential Flow Past an Arbitrary Cascade of Airfoils
Katzoff, S.; Finn, Robert S. & Laurence, James C.
January 10, 1947
Primary view of An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 2: The Effect of Airfoil Section Modifications and the Determination of the Wake Downwash
Anderson, Adrien E.
December 10, 1947
Primary view of An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel Part 5 - Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage TED No. NACA DE308, Part V, Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage, TED No. NACA DE308
Kuhn, Richard E. & Myers, Boyd C., II
October 10, 1947
Primary view of Investigation of the Loads on a Typical Bubble-Type Canopy
Cocke, Bennie W., Jr.
July 10, 1947
Primary view of An Investigation of the Low-Speed Stability and Control Characteristics of Swept-Forward and Swept-Back Wing in the Ames 40- by 80-Foot Wind Tunnel
McCormack, Gerald M. & Stevens, Victor I., Jr.
June 10, 1947
Primary view of Supplementary Data on Airspeeds and Mach Numbers Attained by Lockheed Constellation Airplanes in Transcontinental Operations
Steiner, Roy
October 10, 1947
Primary view of Tuft Studies of the Flow over a Wing at Four Angles of Sweep
Hieser, Gerald
July 10, 1947
Primary view of Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65(sub 112)-111 Airfoil with 35-Percent-Chord Slotted Flap to Determine Pitching-Moment Characteristics and Effects of Roughness
Racisz, Stanley F.
February 10, 1947
Primary view of Yaw Characteristics and Sidewash Angles of a 42 Degree Sweptback Circular-Arc Wing With a Fuselage and With Leading-Edge and Split Flaps at a Reynolds Number of 5,300,000
Salmi, Reino J. & Fitzpatrick, James E.
December 10, 1947
Back to Top of Screen