2,997 Matching Results

Search Results

Advanced search parameters have been applied.

The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. 1.-swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lift and Drag, Mach Number, 1.61

Description: Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61.
Date: March 11, 1955
Creator: Carlson, H. W. & Smith, N. F.
Partner: UNT Libraries Government Documents Department

Investigation of aerodynamic characteristics of an airplane configuration having tail surfaces outboard of the wing tips at Mach numbers of 2.30, 2.97, and 3.51

Description: Aerodynamic characteristics of aircraft configuration having tail surfaces outboard of wing tips at supersonic speeds - wind tunnel stability test.
Date: June 23, 1958
Creator: Church, J. D.; Hayes, W. C., Jr. & Sleeman, W. C., Jr.
Partner: UNT Libraries Government Documents Department

The Origin and Distribution of Supsonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. V - Swept-wing Heavy-bomber Configuration With Large Store Nacelle . Mach Number 2.01

Description: Origin & distribution of supersonic store interference/measurement of individual forces - swept-wing heavy bomber with large store figure.
Date: February 13, 1956
Creator: Carlson, H. W. & Geier, D. J.
Partner: UNT Libraries Government Documents Department