Volume 1. Performance Flight Testing. Appendix F. Derivations.

reportActive / Technical Report | Accession Number: ADA320201 | Open PDF

Abstract:

No Abstract Identified

Author(s):
No Author(s) Identified
Author Organization(s):
AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA
Supplementary Note:
ADA320202 ADA320203 ADA320204 ADA320205 ADA320206 ADA320207 ADA320208 ADA320209 ADA320210 ADA320211 ADA320212 ADA320213 ADA320214 ADA320215 ADA320216 ADA320217 ADA320218 ADA320219 ADA320220 ADA320221 ADA320222 ADA320223 ADA320224
Pagination:
0039

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Monitor Series:
USAF-TPS
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_5.3_Planning; JCA_5_Command and Control; JCA_5.3.1_Analyze Problem
Modernization Areas:
Hypersonics
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
*FLIGHT TESTING, *PERFORMANCE(ENGINEERING), *DERIVATIVES(MATHEMATICS), THERMODYNAMICS, KINETIC ENERGY, GEOMETRY, COURSES(EDUCATION), SOUND WAVES, EULER EQUATIONS, POTENTIAL ENERGY, SUPERSONIC FLOW, ACOUSTIC VELOCITY, TRIGONOMETRY
Field(s)/Group(s):
Aerodynamics, Numerical Mathematics, Manufacturing and Industrial Engineering and Control of Production Systems
Report Date:
1962 Jan 01
Creation Date:
1997 Feb 05