Vols. 3, 7, and 8 published: Lawrence, Kan. : University of Kansas
Text of Note
Includes bibliographical references
NOTES PERTAINING TO TITLE AND STATEMENT OF RESPONSIBILITY
Text of Note
Jan Roskam
ORIGINAL VERSION NOTE
Text of Note
1
Text of Note
2
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
4
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
4
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
4
Text of Note
5
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
4
Text of Note
5
Text of Note
1
Text of Note
2
Text of Note
3
Text of Note
4
Text of Note
5
Text of Note
1
Text of Note
2
CONTENTS NOTE
Text of Note
pt.I. Preliminary sizing of airplanes -- pt.II. Preliminary configuration design and integration of the propulsion system -- pt.III. Layout design of cockpit, fuselage, wing, and empennage, cutaways and inboard profiles -- pt.IV. Layout of landing gear and systems -- pt.V. Component weight estimation -- pt.VI. Preliminary calculation of aerodynamic, thrust, and power characteristics -- pt.VII. Determination of stability, control, and performance characteristics, FAR and military requirements -- pt.VIII. Airplane cost estimation, design, development, manufacturing and operating