A study to determine the accuracy of 2 computer programs in predicting hinge moments for all movable tail fins on missile bodies
Abstract
The preliminary design of a guided missile with movable control surfaces requires an in-depth study of the aerodynamic loading experienced by these surfaces. (Author).
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- May 1983
- Bibcode:
- 1983STIN...8415169S
- Keywords:
-
- Aerodynamic Forces;
- Aerodynamic Loads;
- Computer Programs;
- Control Surfaces;
- Fins;
- Missiles;
- Moments;
- Prediction Analysis Techniques;
- Tail Assemblies;
- Torque;
- Accuracy;
- Angle Of Attack;
- Aspect Ratio;
- Mach Number;
- Tapering;
- Launch Vehicles and Space Vehicles