Comparison and Evaluation of Two Model Techniques Used in Predicting Bomb-Release Motions
Explore the source record for details and available documents.
Carlson, Harry W↗
Engineering topics
Carlson, Harry W
Publications and source records attributed to Carlson, Harry W.
The Aerodynamic Characteristics of a Body in the Two-dimensional Flow Field of a Circular-arc Wing at a Mach Number of 2.01
Explore the source record for details and available documents.
Gapcynski, John P↗
Measurement of static forces on externally carried bombs of fineness ratios 7.1 and 10.5 in the flow field of a swept-wing fight-bomber configuration at a Mach number of 1.6
Explore the source record for details and available documents.
Geier, Douglas J↗
Measurement of Static Forces on Internally Carried Bombs of Three Fineness Ratios in Flow Field of a Swept-wing Fighter-bomber Configuration at a Mach Number of 1.61 with Illustrative Drop-path Calculations
Explore the source record for details and available documents.
Smith, Norman F↗
Experimental techniques for predicting store motions during release or ejection
Explore the source record for details and available documents.
Faget, Maxime A↗
The Origin and Distribution of Supersonic Store Interference from Measurement of Individual Forces on Several Wing-fuselage-store Configurations III : Swept-wing Fighter-bomber Configuration with Large and Small Stores. Mach Number, 1.61
Explore the source record for details and available documents.
Smith, Norman F↗
An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations
Explore the source record for details and available documents.
Carlson, Harry W↗
Some effects of configuration variables on store loads at supersonic speeds
Explore the source record for details and available documents.
Smith, Norman F↗
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations II : swept-wing-heavy-bomber configuration with large store (nacelle). lateral forces and pitching moment
Explore the source record for details and available documents.
Smith, Norman F↗
The origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations I : swept-wing heavy-bomber configuration with large store (nacelle). lift and drag; Mach number, 1.61
Explore the source record for details and available documents.
Smith, Norman F↗
A Pressure-distribution Investigation of the Aerodynamic Characteristics of a Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers of 1.41 and 2.01
The changes in the aerodynamic characteristics of a body of revolution with a fineness ratio of 8 have been determined at Mach numbers of 1.41 and 2.01, a Reynolds number, based on body length, of 4.54 x 10 to the 6th power, and angles of incidence of 0 degrees and plus or minus 3 degrees as the position of the body is varied with respect to a reflection plane. The data are compared with theoretical results.
Gapcynski, John P↗
Preliminary Investigation of the Effects of Body Contouring as Specified by the Transonic Area Rule on the Aerodynamic Characteristics of a Delta Wing-body Combination at Mach Numbers of 1.41 and 2.01
Explore the source record for details and available documents.
Carlson, Harry W↗