Bumblebee Program - aerodynamic data
By: G. A. Barnes and L. L. Cronovich ; prepared for Langley Research Center under contract L-60036A
Contributors: Cronovich, L. L; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA contractor report -- 3114-3117
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va. : For sale by the National Technical Information Service]
Language: eng
Subjects: Guided missiles; Aerodynamics, Supersonic
Notes: Includes bibliographical references
Table of contents: value: pt. 1. Supersonic flow field, pressure field, and panel load data for validation of computational methods; value: pt. 2. Flow fields at Mach number 2.0; value: pt. 3. Pressure fields at Mach numbers 1.5 and 2.0; value: pt. 4. Wing loads at Mach numbers 1.5 and 2.0